118 20 8239 https://digitalprojects.uah.edu/files/original/20/996/spc_stnv_000049.pdf cf77a09b2dab3ca549ff01ac46eeba9a PDF Text Text AERO-ASTRODYNAMICS LABORATORY BIMONTHLY PROGRESS REPORT December 1968 .January 1969 INDEX Page ............................ I1. PROJECTS OFFICE ........................................... I11. ADVANCED STUDIES OFFICE ................................... A . A s t r o d y n a m i c s a n d M i s s i o n A n a l y s i s G r o u p .............. B . Systems A n a l y s i s Group ................................ C . F l i g h t Mechanics and Performance A n a l y s i s Group ....... I V. AEROSPACE ENVIRONMENT DIVISION ............................ A . Space Environment Branch .............................. B . Atmospheric Dynamics Branch ........................... C . T e r r e s t r i a l Environment ............................... V. AEROPHYSICS DIVISION ...................................... A . Mechanical Design O f f i c e .............................. B . Aerodynamic Design Branch ............................ C . Experimental Aerophysics Branch ....................... D . Thermal Environment Branch ............................ E . Unsteady Gas Dynamics Branch .......................... V I. ASTRODYNAMICS AND GUIDANCE THEORY DIVISION ................ A . O p t i m i z a t i o n Theory Branch ............................ B . Astrodynamics Branch ................................ C . Guidance Theory Branch ................................ DYNAMICS AND FLIGHT MECHANICS DIVISION .................... VII. A . S a t u r n V ............................................... B . S a t u r n Apollo A p p l i c a t i o n s Program .................... C . General ................................................ V I I I . FLIGHT TEST ANALYSIS DIVISION ............................. A . S p e c i a l P r o j e c t s O f f i c e and S t a f f ..................... B . F l i g h t E v a l u a t i o n Branch .............................. C . Tracking and O r b i t a l Analysis Branch .................. D . F l i g h t Mechanics Branch ............................... TECHNICAL AND SCIENTIFIC STAFF 3 4 4 5 6 8 8 11 14 15 15 16 22 26 29 32 32 34 37 39 39 42 50 52 52 53 58 61 �AERO-ASTRODYNAMICS LABORATORY BIMONTHLY PROGRESS REPORT December 1968 I. - January 1969 TECHNICAL AND SCIENTIFIC STAFF J - 2 s Program 1. a. Mission Performance Analysis Two-stage p o l a r o r b i t m i s s i o n d a t a w i t h c h i - f r e e z e mode s i m u l a t i o n a r e being p r o c e s s e d . R e s u l t s a r e expected i n t h e near f u t u r e . Design t r a j e c t o r y w i t h o u t c h i - f r e e z e mode was completed and d i s t r i b u t e d t o t h e a p p r o p r i a t e c o n t r a c t o r s . P o l a r o r b i t m i s s i o n d a t a have been g e n e r a t e d u s i n g d i r e c t i n j e c t i o n and Hohmann t r a n s f e r p r o f i l e s f o r o r b i t a l t i t u d e s of 100, 200, and 300 n a u t i c a l m i l e s . Synchronous o r b i t miss i o n d a t a f o r t h e i n - l i n e J - 2 s v e h i c l e (max. t h r u s t J - 2 s ) have been g e n e r a t e d f o r o r b i t i n c l i n a t i o n s of 28.5" and 55" assuming f i v e r e v o l u t i o n s i n t h e 100 n a u t i c a l m i l e parking o r b i t . An e q u a t o r i a l synchronous o r b i t m i s s i o n , one of t h e b a s e l i n e p r o f i l e s , has been r e l e a s e d . The t r a j e c t o r y f o r t h e l u n a r m i s s i o n w i t h d i r e c t i n j e c t i o n i s complete w i t h a payload of 119,000 pounds a s compared t o 110,000 pounds f o r t h e LOR profile (Few) . b . Rendezvous / IGM Guidance Study Some of t h e more s a l i e n t p o i n t s of t h e s t u d y t h u s f a r a r e a s f o l l o w s . T h r o t t l i n g t o 50,000 pounds t h r u s t can improve weight t o o r b i t above d i r e c t b o o s t . S h o r t range rendezvous ( w i t h i n 180" range from launch s i t e ) provides v e r y s m a l l launch windows ( 1 t o 3 min) w i t h IGM c u r r e n t l y formulated can r e l a t i v e l y l a r g e performance p e n a l t i e s . handle moderate c o a s t (300 seconds) w i t h r e v i s e d mission-dependent cons t a n t s , and can a l s o handle t h r o t t l i n g b o o s t p r o f i l e s w i t h moderate range a n g l e s (burn a r c s ) . Three forms of time-to-go e q u a t i o n s i n IGM have been i n v e s t i g a t e d f o r rendezvous w i t h t h r o t t l i n g . The most promising form, which uses launch v e h i c l e and s a t e l l i t e p o s i t i o n and a c c e l e r a t i o n s , has n o t been t e s t e d w i t h lower s t a g e d i s p e r s i o n s . 2. A manuscript e n t i t l e d , "Determination of Meteoroid N a t u r a l Environments from Photographic Meteor Data," has been completed. This i s a r e s u l t of a n o p e r a t i o n s - r e s e a r c h type of e v a l u a t i o n of a l t e r n a t i v e t h e o r e t i c a l and e m p i r i c a l r e s u l t s f o r the physics of meteor f l i g h t i n t h e atmosphere. A p r e l i m i n a r y n e c e s s i t y was t o c o n s t r u c t a mathematical model f o r s e t h e t h e o r e t i c a l r e s u l t s which were published i n 1958 by D r . E r n s t J . Opik from t h e Armagh Observatory i n Northern I r e l a n d . Meteor �luminous e f f i c i e n c y i s t h e r a t i o of the a i r - e n t r y k i n e t i c energy of t h e meteoroid and t h e i n t e g r a t e d luminous i n t e n s i t y of t h e consequent meteor. The c e n t r a l problem was t o determine whether t h e mode-result f o r t h e velocity-and-mass dependence of meteor luminous e f f i c i e n c y was more o r l e s s p l a u s i b l e than any model p r a p o r t i o n a l t o t h a t which is presupposed i n t h e mass s c a l e , which has been used by t h e Harvard Meteor P r o j e c t s i n c e 1438. The a n a l y s i s , c o n t r a r y t o r e c e n t s t u d i e s by D r . Franco V e r n i a n i a t t h e Smithsonian A s t r o p h y s i c a l ObservaLory, shows t h a t , w i t h a c t u a l meteor s t a t i s t i c s , t h e 1958 newer work by Opik is more p l a u s i b l e t h a n t h e 1938 Harvard model, which was bgsed on t h e 1931 o l d e r r e s u l t s , a l s o by g p i k . The consequence is t o i n c r e a s e t h e c a l c u l a t e d v a l u e s of t h e k i n e t i c energy and t h e mass of a f a s t meteor. (Dalton) 3. Experimentation is planned a t MSFC t e s t s i t e s t o measure nearground winds b o t h by tower-mounted anemometers and by a crossed-beam system combining a s i n g l e beam w i t h a multiple-beam d e t e c t o r . A TM X was prepared i n which t h e p e r t a i n i n g beam geometry is s t u d i e d , i t s range of p h y s i c a l a p p l i c a b i l i t y i s examined, and a f i n a l proposal is made f o r a n optimum d e t e c t o r arrangement d e s t i n e d t o observe h o r i z o n t a l winds a t s e v e r a l h e i g h t s s i m u l t a n e o u s l y . . Also, work has been i n p r o g r e s s on a s u i t a b l e single-beam (Heybey) d e t e c t o r l a y o u t f o r measuring non-horizontal winds. 4. Transformations Between D i f f e r e n t Fundamental P l a n e s For many a s t r o n a u t i c a l i n v e s t i g a t i o n s , i t i s n e c e s s a r y t o r e f e r t h e o r b i t of a s p a c e c r a f t , o r a n a t u r a l o r a r t i f i c i a l s a t e l l i t e n o t o n l y t o t h e e q u a t o r i a l p l a n e of i t s ~ g n t r a lp l a n e t b u t a l s o t o t h e o r b i t a l plane of t h e p l a n e t , o r t h e e c l i p t i c , or t h e c e l e s t i a l e q u a t o r , o r even t h e f i x e d , p r o p e r , L a p l a c i a n p l a n e of t h e s a t e l l i t e . When a l l t h e s e fundamental p l a n e s a r e p r o j e c t e d on the c e l e s t i a l s p h e r e , t h e r e a r e 19 s p h e r i c a l t r i a n g l e s . To h e l p t h e a s t r o n a u t i c a l m i s s i o n p l a n n e r , a s y s t e m a t i c c a t a l o g u e has been s e t up which g i v e s 30 independent r e l a t i o n s f o r each of t h e 19 s p h e r i c a l t h i a n g l e s , o r a t o t a l of 570 e q u a t i o n s . Addit i o n a l l y , 5 r e l a t i o n s between d i f f e r e n t i a l s a r e g i v e n f o r each s p h e r i c a l t r i a n g l e , o r a t o t a l of 95 r e l a t i o n s . A t f i r s t , i t was n e c e s s a r y t o f i n d a l s o a s y s t e m a t i c way t o d e s i g n a t e (symbols) t h e q u a n t i t i e s appearing i n t h e many s p h e r i c a l t r i a n g l e s . A t p r e s e n t , i n c l i n a t i o n s and l o n g i t u d e s of nodes, a s w e l l a s t h e i r time r a t e s , a r e compiled f o r t h e d i f f e r e n t p l a n e t a r y and n a t u r a l s a t e l l i t e systems i n our s o l a r system. It is planned t o c a l c u l a t e t h e s e q u a n t i t i e s , r e f e r r e d t o the other reference planes. (Krause) �11. PROJECTS OFFICE 1. The f i f t e e n t h meeting of the Saturn/Apollo F l i g h t Limits subP a n e l (of t h e F l i g h t Mechanics P a n e l ) was h e l d a t MSFC on January 17, 1969. During t h e meeting, two changes f o r AS-504's manual a b o r t l o g i c were recommended. F i r s t change: Use 5 " p i t c h o r yaw a t t i t u d e e r r o r as a f i r s t cue d u r i n g t h e S-IC f l i g h t phase. This provides a n e a r l y cue f o r t h e l o s s of a t t i t u d e e r r o r s i g n a l malfunction. The second a b o r t cue w i l l be t h e d e l t a P i n d i c a t o r . A 5 " r o l l e r r o r w a s a l r e a d y planned a s a f i r s t cue mainly f o r an a c t u a t o r hardover f a i l u r e . Second change: F o r a n S - I C c o n t r o l engine o u t b e f o r e 50 seconds, i g n o r e d e l t a P a s an a b o r t cue. Recent a n a l y s e s i n d i c a t e d t h a t w i t h an S-IC c o n t r o l engine o u t b e f o r e 50 seconds, it i s p o s s i b l e t o exceed t h e d e l t a P l i m i t s (3.2 p s i ) and n o t l o s e c o n t r o l o r exceed t h e s t r u c t u r a l limit. T h e r e f o r e , w i t h o u t t h i s change, i t was p o s s i b l e t o g e t f a l s e a b o r t i n d i c a t i o n s . There a r e no a d d i t i o n a l r i s k s a s s o c i a t e d w i t h t h i s change, s i n c e , a f t e r tower c l e a r a n c e , an engine o u t b e f o r e 50 seconds does n o t r e s u l t i n an a b o r t requirement d u r i n g the max q r e g i o n . The Crew S a f e t y Panel has o f f i c i a l l y approved t h e s e recommendations. D e t a i l e d minutes of t h e meeting a r e documented i n memorandum R-AEROP-S- 2-69. 2. A l t e r n a t e and backup missions f o r t h e AAP CORE program have been i d e n t i f i e d and r e s u l t s p r e s e n t e d t o t h e Mission Requirements Panel. Plans i n c l u d e r e t a i n i n g t h e c a p a b i l i t y f o r f l y i n g a backup CSM/LM/ATM decoupled m i s s i o n i n t h e e v e n t of workshop f a i l u r e and d e l a y i n launching t h e backup workshop. I n a l l c a s e s , however, t h e AAP hardware is used t o o b t a i n , e v e n t u a l l y , t h e c l u s t e r m i s s i o n whereby t h e workshop i s used i n s u p p o r t of t h e astronomy m i s s i o n . The r e s u l t s of t h i s a n a l y s i s a r e t o be p r e s e n t e d a t t h e n e x t b a s e l i n e meeting. 3 . A s t u d y of c o n t r o l l e d r e e n t r y f o r t h e AAP c l u s t e r hardware h a s been completed and r e s u l t s forwarded t o h e a d q u a r t e r s . The s t u d y was performed t o determine t h e f e a s i b i l i t y of c o n t r o l l i n g t h e impact t o a s s u r e p r e v e n t i n g land impact f o r t h e AAP hardware a f t e r t h e AAP-314 m i s s i o n i s completed. R e s u l t s showed t h a t e i t h e r ( a ) a r e t r o - s y s t e m weighing about 4000 pounds o r ( b ) a l i g h t e r system designed f o r operat i o n up t o 600 days a f t e r launch w i t h t h e a t t i t u d e c o n t r o l system and o t h e r onboard systems' l i f e t i m e s i m i l a r l y extended would be n e c e s s a r y . It was concluded t h a t c o n t r o l l e d r e e n t r y f o r t h e AAP c l u s t e r hardware i s impractical . �4. Headquarters has approved t h e p l a n s f o r SPS i n s e r t i o n f o r t h e manned AAP 1, 3A, and 3 v e h i c l e s . his technique improves t h e payload c a p a b i l i t y f o r t h e s e v e h i c l e s by a b o u t 2500 pounds. his improvement s o l v e s t h e b a s i c payload problem b u t does n o t e l i m i n a t e t h e t o t a l problem because o i t h e l i m i e a t i o h s impdsed on t h e CM by t h e paracljutehung ,weight. During a b o r t , t h e CM i s a t t h e parachute l i m i t of 13,000 he weight Bnd volume l i m i t a t i o n s of t h e CM a r e producing pounds. s e r i o u s s t o r a g e brobleins e s p e c i a l l y f o r t h e 56-day AAP 3A and 3 v e h i c l e s . A. A s trodynamics and M i s s i o n Analysis Group , Miss i o h d e s i g n c h a r t s f o r e a r t h - d e p a r t enkrgiqd ~ u h i t e r passage d a t e s and d i s t d d c e s , ~ a t d r r ipadsdge coriditions, an8 ~ l u t o a r r i v a l d a t e s have been com$leted, Theiie e h a r t s and t r ~ j e c t a r yd a t a a r e being prepdred f o r documentation. + 2. Saturn V FSSI~PS~ n t e g r a t i o nStudy A mid- term review of t h e "Saturn V Future Space S t a t i o n / Nuclear-Thermal E l e c t r i c Power Systetn h t e g r a t i o n sttidyti Qas p r e s e n t e d on December 11, 1968; A model f o r t h e rekctor-induced r a d i a t i o n e d i r o n m e n t about t h e s p a c e s t a t i o n , which has been .teceived from Atoinics I h t e t n a t i o n a l C o r p o r d t i o n , i s b e i n g uhed t o ifikbki-8ke t h e t o & I r a d i a t i o n dbde i n c u r r e d along t h e v a r i o u s &emote experimeht module placement and r e t t i e v a l t r a j e c t o r i e s . The p o s s i b i l i t y 04 u s i n g t r a j e c t o r i e s f o r o b t - o f - o r b i t - p l a n e remote experiment module pldkemeht i s being i n v e s t i g a t e d . A p a r a m e t r i c a n a l y s i s f o r v a r i o u s types of t r a j e c t o r i e s v i t h r e s p e c t t o AV budget; t r i n k f e r time, and r a d i a t i o n dose is a l s o being conducted. A f i n a l review of t h e s t u d y ks scheduled f o r mid-March 1969. 3. ITCC Meeting The s e v e n t h mekting of t h e NASA I n t e r p l a n e t a r y T r a j e c t o r y Coordinating Committee was h e l d December 4 and 5 , 1968, a t ~ a n ~ l e ~ Research C e n t e r . The minutes of t h i s meeting a r e a v a i l a b l e . �4. Computer Program Development A matched conic computer program has been developed which matches t h e p l a n e t o c e n t r i c h y p e r b o l i c t r a j e c t o r i e s w i t h t h e h e l i o c e n t r i c t r a j e c t o r y a t t h e s p h e r e of i n f l u e n c e . The program provides p r e l i m i n a r y d a t a f o r communication d i s t a n c e s and o r i e n t a t i o n a n g l e s f o r i n t e r p l a n e t a r y m i s s i o n s , and good i n i t i a l c o n d i t i o n s f o r t h e JPL "Space Tra j e c t o r i e s Program." B. Systems Analysis Group 1. I n t e g r a l Launch and Reentry Systems I n t e g r a l Launch and Reentry Systems (ILRS) s t u d y c o n t r a c t s have been f i n a l i z e d . MSFC has two c o n t r a c t s under i t s d i r e c t i o n : (1) Lockheed M i s s i l e s and Space Company of Sunnyvale, C a l i f o r n i a , and (2) General Dynamics Convair of San Diego, C a l i f o r n i a . MSC has North American Rockwell Corporation of Downey, C a l i f o r n i a , under c o n t r a c t and Langley Research Center has M c ~ o n n e l l / ~ o u g l aCs o r p o r a t i o n of S t . Lous, M i s s o u r i . O r i e n t a t i o n f o r t h e MSFC c o n t r a c t o r s b e g i n s February 18, 1969. The s t u d y p e r i o d has been compressed from e i g h t t o s i x months. Data from t h e ILRS s t u d y a r e t o be f e d i n t o t h e Phase B s t u d y of t h e 1975 Space S t a t i o n . A follow-on s t u d y is t o be l e t immediately a f t e r t h e c u r r e n t ILRS s t u d y is completed. A meeting w i l l be s e t up between t h e c o n t r a c t o r s and MSFC r e p r e s e n t a t i v e s a t t h e February 1 8 c o n t r a c t o r o r i e n t a t i o n . 2. Launch Vehicles The f i r s t review of t h e "Saturn V D e r i v a t i v e (S-1C/S-IVB) Launch Vehicle Systems Study" (NAS8-30506)was h e l d a t MSFC on J a n u a r y 16, 1969. The r e s u l t s r e p r e s e n t e d t h e Phase I t r a d e s t u d y p o r t i o n c o n s t i t u t ing approximately 15 p e r c e n t of t h e t o t a l e f f o r t . The o b j e c t i v e of t h i s phase of t h e s t u d y was t o provide t r a d e d a t a f o r t h e s e l e c t i o n of a basel i n e INT-20 launch v e h i c l e c o n f i g u r a t i o n f o r t h e Phase I1 p r e l i m i n a r y d e s i g n . The t r a d e s included t h e number of engines i n t h e f i r s t s t a g e , s e r i e s of S-IVB s t a g e , s e r i e s of I U , payload envelope, and t h e a x i a l a c c e l e r a t i o n l i m i t . The t e c h n i c a l panel managing t h e c o n t r a c t s e l e c t e d (1) f o u r a v e h i c l e f o r t h e d e s i g n phase w i t h t h e s e c h a r a c t e r i s t i c s : F-1 engines i n t h e S-IC s t a g e , (2) 500 s e r i e s of S-IVB s t a g e and IT, (3) a c a p a b i l i t y of 4 - 6 8 g ' s w i t h a 1 . 4 f a c t o r of s a f e t y , and ( 4 ) t h e payload envelope c o n s i s t i n g of a double a n g l e MLV nose cone and a 43-foot c y l i n d r i c a l s e c t i o n . The s e l e c t e d c o n f i g u r a t i o n w i l l p l a c e 132,000 pounds i n t o a 1 0 0 - n a u t i c a l - m i l e c i r c u l a r o r b i t (payload d e n s i t y of 16.3 l b s / f t 3 ) and is designed t o f l y through March winds. The �b a s e l i n e v e h i c l e i s a l s o capable of c a r r y i n g a 68-foot c y l i n d r i c a l s e c t i o n (payload d e n s i t y of 7.8 l b s / f t 3 ) f l y i n g through t h e August synthetic profile. C. F l i g h t Mechanics and Performance Analysis Group I. Launch Vehicle The f o l l o w i n g memoranda on performance were published during t h i s period: (a) R-AERO-X-68-43, "Performance and T r a j e c t o r y Data f o r t h e T i t a n I I I D Vehicle," December 1 2 , 1968. (b) R-AERO-X~68-44, "Performance and T r a j e c t o r y Data f o r t h e T i t a n I I I C Vehicle," December 20, 1968. (c) R-AERO-X-69-1, "Performance gnd T r a j e c t o r y Data f o r t h e T i t a n IIIM Vehicle," J a n u a r y 1, 1969. Performance d a t a now being g e n e r a t e d f o r t h e T i t a n I I I D Agena and t h e T i t a n IIID-Centaur w i l l be documented l a t e r . 2. S a t u r n V Workshop The Bo concept ( t h e u s e of t h e wet workshop backup a s a d r y workshop launched on a S a t u r n V), which was p r e s e n t e d t o D r . von Braun on December 13, 1968, i s being documented. From t h i s meeting evolved the concept of t h e S a t u r n V c l u s t e r m i s s i o n , a g r o u n d - f i t t e d S-IVB workshop launch on a S a t u r n V and l a g i s t i c a l l y supported w i t h S a t u r n I B f l i g h t s . This was conceived a s a replacement f o r t h e core program. It was p r e s e n t e d go D r . Lucas pn January 29, 1969, and i s t o b e completed and p r e s e n t e d t o D r . von Brgun on February 26, 1969. Four p o s s i b l e m i s s i o n p r o f i l e s were g e n e r a t e d . F i r s t considered was t h e p o s s i b i l i t y of u s i n g a BL I1 CSM t o t a k e t h e crew up and then r e t u r n t h e f o l l o w i n g day w i t h t h e p r e v i o u s crew, I n t h i s method of o p e r a t i o n , t h e f i r s t BL I1 CSM is thrown away, and t h e l a s t crew d e o r b i t s i n a r e t u r n module t h a t was brought up w i t h t h e workshop on t h e S a t u r n V. There a r e two major d i s a d v a n t a g e s t o t h i s method of o p e r a t i o n : F i r s t , s h o r t pad turn-around time i s r e q u i r e d , and second, i f a crew must r e t u r n e a r l y , they have t o use t h e r e t u r n module intended f o r t h e t h i r d crew and t h e e n t i r e m i s s i o n i s the'reby a b o r t e d . This problem is a l l e v i a t e d i f , i n s t e a d of a BL I1 CSM, a modified CSM i s useg, t h e major m o d i f i c a t i o n being t h e i n s e r t i o n of q s o l i d r e t r o - p a c k between t h e command and s e r v i c e module. This gllows t h e s e r v i c e module w i t h i t s l i m i t e d l i f e t i m e t o be d i s c a r d e d a f t e r docking w i t h t h e workshop. S i n c e t h e crews r e t u r n i n t h e command module that took them t o o r b i t , t h e ~ ei s no requirement f o r crew o v e r l a p , and t h e crews may be spaced as d e s i r e d . �I n each of t h e s e m i s s i o n p r o f i l e s , t h e LM/ATM i s brought up by a S a t u r n I B launched a f t e r t h e t h i r d crew, and an unmanned rendezvous and dock a r e done w i t h t h e LM. The o t h e r two m i s s i o n s ' p r o f i l e s e l i m i n a t e t h e need f o r t h i s e x t r a f l i g h t and the LM by launching t h e ATM a s p a r t of t h e workshop on the S a t u r n V. There is a p o s s i b i l i t y of a d e c i s i o n soon concerning t h i s configuration. 3. Nuclear This o f f i c e has been r e q u e s t e d by R-AS-MP t o a s s i s t i n a S a t u r n nuclear launch v e h i c l e f l i g h t s a f e t y s t u d y f o r SNPO. The c a p a b i l i t y , i n c a s e of an a b o r t a f t e r d e p a r t u r e from c i r c u l a r o r b i t , of t h e n u c l e a r s t a g e t o i n j e c t onto a n i n t e r m e d i a t e e l l i p s e f o r a twoyear minimum l i f e t i m e i s being analyzed. 4. Unmanned P l a n e t a r y Performance d a t a f o r s e v e r a l p o s s i b l e Grand Tour m i s s i o n launch v e h i c l e c o n f i g u r a t i o n s have been g e n e r a t e d . The S a t u r n V p e r formance was based on t h e SA-502 launch v e h i c l e which i n c o r p o r a t e s J - 2 s engines i n t h e upper s t a g e . The c o n f i g u r a t i o n s s t u d i e d included t h e b a s i c S a t u r n V, S a t u r n VINuclear, S a t u r n V/Service Module, S a t u r n V/ Centaur, and t h e S a t u r n V w i t h an assumed s p a c e c r a f t p r o p u l s i o n system used f o r i n j e c t i o n . The INT-20/Service Module and I N T - 2 0 / ~ e n t a u r c o n f i g u r a t i o n s were a l s o s t u d i e d , w i t h t h e e f f e c t s of i n c l u d i n g t h e 3 - 2 s engine i n t h e S-IVB being determined f o r b o t h c o n f i g u r a t i o n s . 5. Launch Vehicle T r a j e c t o r y Optimization Computer Program With o n e - t h i r d of t h e c o n t r a c t p e r i o d f i n i s h e d , work b e i n g done by Northrop on t h e Launch Vehicle T r a j e c t o r y O p t i m i z a t i o n Computer Program (Phase IV) i s p r o g r e s s i n g v e r y w e l l ; i t looks now a s i f we w i l l g e t a l l t h a t was expected from t h e c o n t r a c t . 6. ROBOT The ROBOT t r a j e c t o r y o p t i m i z a t i o n program has been modified t o g r e a t l y reduce t h e p r i n t o u t . This r e s u l t s i n s u b s t a n t i a l s a v i n g s i n computer paper and time r e q u i r e d f o r p r i n t i n g t r a j e c t o r i e s r u n f o r t h i s o f f i c e by t h e Computation Laboratory, �IV. AEROSPACE ENVIRONMENT DIVISION A, Space Environment Branch 1. Atmospheric Model S t u d i e s The d e t a i l e d s t u d y program f o r t h e development of an improved upper atmospheric model is c o n t i n u i n g , C u r r e n t s t u d i e s i n s u p p o r t of t h i s program a r e b o t h s t a t i s t i c a l and t h e o r e t i c a l . I n t h e s t a t i s t i c a l s t u d i e s , drag-determined d e n s i t i e s from 64 s a t e l l i t e s a r e being used t o develop r e g r e s s i o n e q u a t i o n s t h a t d e f i n e t h e atmospheric d e n s i t y i n terms of e x o s p h e r i c temperature ( c a l c u l a t e d from ~ a c c h i a ' se q u a t i o n s ) a t d i s c r e t e a l t i t u d e l e v e l s from 140 t o 350 km. S i m i l a r equatiohd w i l l a l s o be e s t a b l i s h e d f o r a l t i t u d e l e v e l s below 140 km u s i n g c l a s s i f i e d , l o w - a l t i t u d e , A i r Force s a t e l l i t e drag d e n s i t y d a t a and i n f o r m a t i o n t h a t might be i n f e r r e d from t h e a l t i t u d e dependency of t h e r e g r e s s i o n c o e f f i c i e n t s obtained i n t h e above 140 km s t u d i e s . These e q u a t i o n s w i l l be used t o develop a aiodel of t h e atmospheric mass d e n s i t y from 90 t o 1000 km a l t i t u d e , The new model w i l l provide p r e d i c t i o n s of atmospheric d e n s i t y t h a t a r e i n b e t t e r agreement w i t h s a t e l l i t e drag d e n s i t i e s than t h e p r e d i c t i o n s obtained from c u r r e n t atmosp h e r i c models. These s t u d i e s a r e being conducted j o i n t l y w i t h in-house NASA e f f o r t and under Lockheed M i s s i l e s and Space Company c o n t r a c t NAS8-30513. The s t a t i s t i c a l s t u d i e s d i s c u s s e d i n t h e above paragraph w i l l r e s u l t i n an improved atmoepheric d e n s i t y model, b u t t h e y w i l l not provide i n f o r m a t i o n r e l a t F v e t o atmospheric temperature and chemical composition. To o b t a i n t h i s i n f o r m a t i d n , v a r i o u s t h e o r e t i c a l s t u d i e s a r e being conducted t o e s t a b l i s h a model atmosphere t h a t w i l l be cons i s t e n t w i t h t h e mass d e n s i t i e s of the model d i s c u s s e d above and t h a t w i l l a l s o be i n agreement w i t h e x i s t i n g temperature and chemical comp o s i t i o n measurements. I n one s u c h s t u d y , a new technique f o r c a l c u l a t i n g t h e temperature and O2 and 0 number d e n s i t i e s t h a t should be a s s o c i a t e d w i t h measured N 2 d e n s i t y p r o f i l e s has been e s t a b l i s h e d . The technique has been a p p l i e d t o M2 p r o f i l e s obtained from s i x M a r s h a l l / u n i v e r s i t y of Mighican Probes (MUMP) t h a t were launched i n s e r i e s from Cape Kennedy on January 24, 1967. The c a l c u l a t e d O2 and 0 number d e n s i t i e s a r e i n e x c e l l e n t agreement w i t h o t h e r e x i s t i n g mass s p e c t r o m e t e r and a b s o r p t i o n s p e c t r o m e t e r measurements. The newly developed technique and t h e r e s u l t ing atmospheric i n f o r m a t i o n a r e d i s c u s s e d i n a paper e n t i t l e d , "Diurnal y V a r i a t i o n i n t h e Thermosphere from a S e r i e s of ~ a r s h a l l / ~ n i v e r s i tof Michigan Probes." The paper has been s e n t t o t h e J o u r n a l of Geophyeical Research f o r p u b l i c a t i o n . �~ a c c h i a ' sexospheric temperature equations a r e being mod i f i e d t o make them more c o n s i s t e n t w i t h e x o s p h e r i c t e m p e r a t u r e s t h a t have b e e n o b t a i n e d from t h e MUMP program. When e s t a b l i s h e d , t h e s e e q u a t i o n s w i l l be used i n c o n j u n c t i o n w i t h t h e improved d e n s i t y model t o c a l c u l a t e atmospheric chemical composition. R e s u l t s from a l l o f t h e s e w i l l b e used t o e s t a b l i s h a n improved dynamic upper a t m o s p h e r i c model. The f i n a l v e r s i o n of t h i s model w i l l d e f i n e t h e a t m o s p h e r e from 90 t o 1000 km a l t i t u d e and w i l l n o t b e l i m i t e d b y c o n s t a n t 1 2 0 km boundary c o n d i t i o n s o r s t a t i c d i f f u s i o n a s s u m p t i o n s which a r e i n h e r e n t i n t h e c u r r e n t models. 2. Environment C r i t e r i a The monograph e n t i t l e d , " E a r t h O r b i t a l Atmospheric Model," w i l l be p u b l i s h e d by t h e O f f i c e of Advanced R e s e a r c h and Technology a s a NASA S p e c i a l P u b l i c a t i o n . S p e c i a l i z e d environment c r i t e r i a i n p u t s , n o t g i v e n i n NASA TM X-53798, "Space Environment C r i t e r i a G u i d e l i n e s f o r Use i n Space V e h i c l e Development, 1968 R e v i s i o n , " have b e e n f u r n i s h e d t o s e v e r a l e n g i n e e r i n g and s c i e n t i f i c s t u d i e s i n s u p p o r t of t h e OWS/ATM and F u t u r e Space S t a t i o n (FSS) programs. To f u r n i s h t h e s e s p e c i a l i z e d e n v i r o n m e n t c r i t e r i a i n a more s y s t e m a t i c manner, a document e n t i t l e d , " V a r i a t i o n i n Atmospheric D e n s i t y f o r MSFC 1971-1976 O r b i t a l Space S t a t i o n Programs," h a s b e e n w r i t t e n . The document, w h i c h w i l l b e p u b l i s h e d a s a NASA TM X i n F e b r u a r y 1969, w i l l a s s i s t t h e u s e r i n d e t e r m i n i n g t h e environment c r i t e r i a r e q u i r e m e n t s f o r a p a r t i c u l a r e n g i n e e r i n g o r s c i e n t i f i c s t u d y . It w i l l a l s o p r o v i d e p r e d i c t i o n s of t h e mean o r b i t a l a t m o s p h e r i c d e n s i t y , p r e s s u r e , and m o l e c u l a r w e i g h t t o which a s p a c e c r a f t w i l l b e exposed on p a r t i c u l a r days a t i n t e r v a l s of t h r e e months from J a n u a r y 1, 1971 t h r o u g h J a n u a r y 1, 1977. 3. Solar Activity Studies Lockheed M i s s i l e s and Space Company h a s computed c r o s s c o r r e l a t i o n f u n c t i o n s f o r s u n s p o t s and e a c h of t e n s e l e c t e d p r e d i c t o r s , which a r e d e s c r i p t i v e of t h e i n t e r a c t i o n of t h e p l a n e t s w i t h t h e s u n . P r e d i c t o r s t a k e n a t t h e time of s u n s p o t numbers p l u s a time z have b e e n used t o o b t a i n t h e v a l u e of T t h a t g i v e s t h e maximum and minimum c r o s s c o r r e l a t i o n f u n c t i o n s f o r .c # 0. T h i s i n f o r m a t i o n w a s t h e n used t o c a l c u l a t e c o r r e l a t i o n c o e f f i c i e n t s . The b e s t c o r r e l a t i o n s were o b t a i n e d by t r e a t i n g t h e s u n s p o t s a s a c y c l e of 22 y e a r s r a t h e r t h a n 11 y e a r s . The 22-year c y c l e c o n s i d e r s t h e f i r s t h a l f o f t h e c y c l e p o s i t i v e and t h e l a s t h a l f n e g a t i v e . These p r e d i c t o r s a r e b e i n g s u b j e c t e d t o a nonl i n e a r c o r r e l a t i o n t e c h n i q u e t o g i v e a s u n s p o t p r e d i c t i o n method. �MIT Experimental Astronomy Laboratory is c o n t i n u i n g r e s e a r c h f o r p o s s i b l e p l a n e t a r y e f f e c t s on t h e sun. ~ a b c o c k ' s h y p o t h e s i s of a p h y s i c a l model of t h e sun which would permit t h e formation of s u n s p o t s by p l a n e t a r y i n f l u e n c e s i s being s t u d i e d . Some of t h e s e hypotheses a r e being v e r i f i e d ; i t i s hoped t h a t t h e p l a n e t a r y t i d a l f o r c e caq be shown t o be a t l e a s t p a r t of t h e s u n s p o t t r i g g e r i n g mechanism. The proposed c o n t r a c t w i t h t h e S o l a r A c t i v i t y Group of t h e ESSA Space D i s t u r b a n c e Labotatory f o r D r . S l u t z t o s t u d y s o l a r a c t i v i t y i s s t i l l being n e g o t i a t e d . 4. A L i n e a r Regression S o l a r Cycle Study An in-house s t u d y u s i n g a l i n e a r r e g r e s s i o n technique w i t h monthly d a t a i n d i c a t e s a second peak of s o l a r c y c l e 20 o c c u r r i n g about September 1969. During t h i s expected i n c r e a s e i n s o l a r a c t i v i t y , t h e r e w i l l be an i n c r e a s e d p r o b a b i l i t y of major s o l a r f l a r e s o c c u r r i n g near September 1969. 5. Space S t a t i o n I o n o s p h e r i c Experiment Package The Phase A in-house s t u d y of i o n o s p h e r i c experiments which can be performed from a manned s p a c e s t a t i o n has been completed. A b r i e f i n g of t h e r e s u l t s , t o be g i v e n a t NASA Headquarters on January 30, 1969, w i l l i n c l u d e i n t e r e s t e d groups from MSFC, MSC, Langley and NASA Headquarters. The groups from Headquarters w i l l i n c l u d e r e p r e s e n t a t i v e s of OMSF, OART, and OSSA. A meeting was held w i t h D r . S t u h l i n g e r on January 28, 1969, i n which he was a p p r i s e d of t h e i o n o s p h e r i c experiment s t a t u s . A meeting w i l l be h e l d w i t h D r . E . R. Schmerling, C h i e f , I o n o s p h e r i c P h y s i c s , on January 29, 1969, t o review t h e s t a t u s of t h e experiment package. 6. A c o u s t i c G r a v i t y Wave Study The review of AVCO's f i n a l r e p o r t on Phase I of t h i s s t u d y should be held w i t h i n t h e n e x t two weeks. The Phase I1 c o n t r a c t n e g o t i a t i o n s a r e now i n p r o g r e s s . The Phase I1 emphasis w i l l be placed on o b t a i n i n g l i m i t e d d a t a on times of s t a t i c t e s t f i r i n g s and m e t e o r o l o g i c a l e v e n t s , The a n a l y s is and a s s o c i a t e d s t u d i e s w i l l emphasize t h e coupling of n e u t r a l motions t o i o n o s p h e r i c e l e c t r o n motions and an in-depth s t u d y of t h e a t t e n u a t i o n of a n a c o u s t i c g r a v i t y wave a s i t propagates from t h e t r o p o s p h e r e t o t h e thermosphere. I n a d d i t i o n t o t h e i o n o s p h e r i c sounder d a t a , we w i l l r e q u i r e p e r i o d i c o v e r n i g h t monitoring and p i c t u r e s from t h e weather r a d a r a t t h e Atmospheric Research F a c i l i t y . These w i l l be r e q u i r e d when n i g h t t i m e storm c e l l s a r e f o r e c a s t f o r t h e immediate a r e a . This i s a n OSSA sponsored and funded e f f o r t . �7. I o n o s p h e r i c Monitoring Equipment I n a d d i t i o n t o the MSFC ionosonde, a Phase P a t h Sounder i s being a c q u i r e d f o r use i n subsequent i o n o s p h e r i c experiment programs. This item w i l l r e q u i r e c o n s i d e r a b l e a t t e n t i o n t o o p e r a t i o n and maintenance, s i n c e i t i s a s t a t e - o f - t h e - a r t development. These two p i e c e s of i o n o s p h e r i c monitoring equipment provide a unique o p p o r t u n i t y f o r s t u d y i n g i o n o s p h e r i c dynamics i n c o n s i d e r a b l e d e t a i l . The b u i l d e r s of t h e Phase P a t h Sounder (IT&T) have been c o n t r a c t e d t o come t o MSFC t o t r a i n our e n g i n e e r i n g personnel i n t h e r o u t i n e o p e r a t i o n and maintenance of t h i s p i e c e of equipment. The i o n o s p h e r i c experiments subs e q u e n t l y r u n w i l l then depend d i r e c t l y on t h e a v a i l a b i l i t y and c a p a b i l i t y of t h e s e t r a i n e d people. B . Atmospheric Dynamics Branch 1. Technical Meeting Concerning Wind Loads on B u i l d i n g s and S t r u c t u r e s M r . George H. F i c h t l and M r . John W. Kaufman, R-AERO-YE, gave a p r e s e n t a t i o n a t t h e t e c h n i c a l meeting on wind l o a d s on b u i l d i n g s and s t r u c t u r e s , sponsored by t h e Building Research D i v i s i o n , N a t i o n a l Bureau of S t a n d a r d s , and t h e Environmental Data S e r v i c e , ESSA. The purpose of t h e meeting was t o g a t h e r t o g e t h e r a u t h o r i t i e s i n s t r u c t u r a l d e s i g n and atmospheric s c i e n c e t o d i s c u s s t h e wind load problem and perhaps make some s p e c i f i c recommendations t o improve t h e U. S. S t r u c t u r a l B u i l d i n g Code. The meeting covered f o u r a r e a s : (1) e n g i n e e r i n g problems i n t h e d e s i g n of s t r u c t u r e s t o r e s i s t wind l o a d s , ( 2 ) atmosp h e r i c c o n s i d e r a t i o n s , ( 3 ) experimental and t h e o r e t i c a l d e t e r m i n a t i o n of aerodynamic f o r c e s , and (4) r e c e n t advances i n d e s i g n procedures and c u r r e n t d i f f i c u l t i e s . The NASA ground wind d e s i g n wind model f o r KSC and t h e NASA 150 m M e t e o r o l o g i c a l Tower were d e s c r i b e d i n a pres e n t a t i o n by M r . F i c h t l and M r . Kaufman. The approach taken by NASA t o s p e c i f y t h e ground wind environment from a d e s i g n p o i n t of view was w e l l r e c e i v e d . P r o f e s s o r G i l l of t h e Michigan S t a t e U n i v e r s i t y , a well-known a u t h o r i t y on i n s t r u m e n t a t i o n , pointed o u t t h a t t h e NASA 150 m M e t e o r o l o g i c a l Tower is one of t h e f i n e s t towers of i t s kind i n t h e U. S. and i s an example of what can be done. Furthermore, he pointed o u t t h a t t h e d a t a from t h i s tower should be used i n t h e new U . S. Building Code t o s p e c i f y wind flow c o n d i t i o n s over "Type C" t e r r a i n . It appears t h a t t h e NASA Tower F a c i l i t y and a n ESSA F a c i l i t y a r e t h e only towers i n t h e U . S. t h a t a r e being used t o o b t a i n atmospheric wind d a t a on a r o u t i n e 24-hour b a s i s f o r t h e e x p r e s s purpose of determining wind load f o r c i n g f u n c t i o n s . �The o v e r a l l approach t o t h e wind problem by NASA w a s h a i l e d a s being a p o s i t i v e s t e p forward t o o b t a i n i n g a s o l u t i o n t o t h e wind load problem. The work performed by Marshall personnel i n ground wind environment s p e c i f i c a t i o n i s a b e n e e i c i a l by-product of t h e aerospace indus t r y . 2. F i n a l Report under C o n t r a c t NAS8-21148 The f i n a l r e p @ r t has been r e c e i y e d and accepted under C o n t r a c t NAS8-21548, e n t i t l e d , "Studies of V e r t i c a l Wind V e l o c i t y a t Cape Kennedy, F l o r i d a . " The r e p o r t , being published a s a NASA CR, w i l l be a v a i l a b l e soon. VariouB d e t a i l s of wind phenomena a s measured by t h e FPS-16 r a d a r l f i m s p h e r e system, i n c l u d i n g s p e c t r a l energy of t h e mesoand m l c r o - s c a l e v e l o c i t y v a r i a t i o n s , a r e d i s c u s s e d . 3, Study of V e h i ~ l eExhaust Cloud Phenomena A s t u d y e n t i t l e d , "Rise Rate and Growth of S t a t i c T e s t Vehicle Engine Exhaust Clouds ," i s included i n t h e r e c e n t l y published TM X-53782. AEC, A i r Force, a s w e l l a s o t h e r concerns, a r e i n t e r e s t e d i n such d a t a t o s t u d y atmospheric d e b r i s f a l l b a c k , f a l l o u t , i n d u s t r i a l pollution, etc. 4. Revised Ground Wjnd C r i t e r i a Memorppdum R-AERO-YEd176-69, dated January 1 0 , 1469, d i s c u s s e s t h e d i s t r i b u t i o n of peak gxound wipd p r o f i l e shapes Eor m i s s i o n planning and o p e r a t i o n s , Any camments o r q u e s t i o n s r e g a ~ d i n gt h e s e new c r i t e r i a should be d i r e c t e d t o M.P. George F i c h t l of R-AERO-YE, o r Mr. W. W. Vaughan, R-AERO-Y. These c r i t e r i a have been ahd w i l l be used i n t h e f u t u r e i n m o n i t o r i n g wind p r o f i l e c o n d i t i o n s d u r i n g p r e - f l i g h t o p e r a t i o n s of A p o l l o / S a t u r n v e h i c l e s . This work is accomplished by t h e HOSC/MSFC wind monitoriqg team of which MSBCIMSC personnel a r e members. 5 . Jimsphere Ascent Rate Data R e c e n t l y , t h e l o c a l inhouse Boeing c o n t r a c t o r personnel submhtred a d r a f t r e p o r t oh a scheme t o p r o p e r l y f i l t e r the S i m p h e r e a s c e n t r a t e d a t a . The technique d i s c u s s e d i n t h e r e p o r t w i l l be s e r i o u s l y considered a s a d a t a r e d u c t i o n s u b r o u t i n e t o provide r e l i a b l e a s c e n t r a t e d a t a f o r r e s e a r c h of v e r t i c a l wind motion s t u d i e s of t h e upper atmosphere t o a h e i g h t of about 18 km. 6. Atmospheric Turbulence (Ground Winds) a . I n v e s t i g a t i o n @£ t h e t u r b u l e n t wind f i e l d below 500 f t a l t i t u d e a t t h e E a s t e r n T e s t Range, F l o r i d a (Contract NAS8-21140 w i t h t h e Pennsylvania S t a t e U n i v e r s i t y ) . �The f i r s t year of e f f o r t i n t h i s a r e a has been comp l e t e d , and the c o n t r a c t o r has submitted a p r e l i m i n a r y d r a f t of h i s f i n a l r e p o r t f o r review. This r e p o r t covers (1) a n a l y s e s of s p e c t r a of t h e h o r i z o n t a l wind components; ( 2 ) t h e r e l a t i o n between t h e t u r b u l e n t wind components a t d i f f e r e n t h e i g h t s a s manifested by t h e cospectrum o r q u a d r a t u r e spectrum, o r r a t h e r the s p e c t r a l coherence and t h e s p e c t r a l eddy s l o p e ; (3) a p r e l i m i n a r y s t u d y of t h e p r o b a b i l i s t i c s t r u c t u r e of t u r b u l e n t f o r c i n g of launch v e h i c l e s ; and (4) t h e q u a s i - s t e a d y wind p r o f i l e . Although much i n f o r m a t i o n about atmospheric t u r b u l e n c e has been gained d u r i n g t h i s f i r s t year of e f f o r t , t h e r e i s much t o l e a r n ; t h e r e f o r e , t h i s c o n t r a c t w i l l be continued f o r a n o t h e r y e a r . The cont r a c t o r w i l l g i v e a b r i e f i n g on h i s work i n l a t e February. b. Ground wind f i e l d a n a l y s i s f o r d e s i g n and o p e r a t i o n f o r s p a c e v e h i c l e s (NAS8-21178 C o r n e l l A e r o n a u t i c a l L a b o r a t o r i e s , I n c . ) . This e f f o r t w i l l be completed i n mid-February. The c o n t r a c t o r has completed h i s d a t a a n a l y s e s , and a f i n a l r e p o r t i s now b e i n g d r a f t e d . We should r e c e i v e t h i s r e p o r t i n e a r l y February f o r review and comments. The r e p o r t w i l l be concerned w i t h q u a s i s t e a d y wind p r o f i l e s , g u s t f a c t o r s , g u s t a c c e l e r a t i o n s , s p e c t r a , e t c . The c o n t r a c t o r w i l l g i v e a b r i e f i n g on h i s work i n l a t e February. c . Ground Wind Turbulence Analys i s (In-House E f f o r t ) A d e s i g n s p e c t r a l model was completed d u r i n g t h i s The r e s u l t s of t h i s e f f o r t and o t h e r a s p e c t s of t h e ground wind period. problem were p r e s e n t e d i n a paper by M r . F i c h t l and M r . Kaufman a t t h e NBS-ESSA meeting on wind l o a d s on b u i l d i n g s and t a l l s t r u c t u r e s i n Washington, D. C . on January 27 and 28. The paper was w e l l r e c e i v e d . M r . F i c h t l and D r . John Dutton of t h e Pennsylvania S t a t e U n i v e r s i t y submitted a paper e n t i t l e d "Approximate Equations of Motion f o r Gases and L i q u i d s , " t o t h e J o u r n a l f o r Atmospheric Sciences. The p a p e r , which w i l l appear i n t h e March e d i t i o n , i s concerned w i t h developing a cons i s t e n t s e t of Boussinesq approximated e q u a t i o n s f o r f l u i d flotqs i n g r a v i t a t i o n a l l y s t r a t i f i e d f l u i d s . These e q u a t i o n s a r e being used i n some of t h e a n a l y s e s of low l e v e l atmospheric t u r b u l e n c e and wind p r o f i l e s . 7. A n a l y s i s of Atmospheric Turbulence from FPS-16 ~ a d a r / Jimsphere Data (NAS8-21331 w i t h t h e Meteorology Research, Incorporated) The c o n t r a c t o r has completed most of t h e work on t h i s f i r s t year of e f f o r t . The r e s u l t s seem t o show t h a t t h e FPS-16 ~ a d a r l ~ i m s p h e r e system might be capable of d e t e c t i n g c l e a r a i r t u r b u l e n c e . A f i n a l r e p o r t �w i l l be prepared i n February. Although e x t e n s i v e work has been done d u r i n g t h e f i r s t y e a r , t h e r e is much l e f t t o be done. Accordingly, t h i s e f f o r t sill be renewed f o r an a d d i t i o n a l y e a r . 8. Operation Procedures f o r Determining Space Vehicle Response t o Wind Turbulence (NAS8-21325 w i t h t h e Martin-Marietta Corporation) M r . F i c h t l , R-AERWYE, t r a n s m i t t e d quas i-s teady wind and t u r b u l e n c e s p e c t r a s t a t i s t i c s of i n - f l i g h t winds t o Mrs. ~ l b e r t aKing, R-AERO-DD, t h e c d n t r a c t monitor. These s t a t i s t i c s w i l l be used t o develop a p r e l a u n c h m o n i t a r s h i p l o a d s f o k e c a s t i n g procedure and t o s t u d y load s e n s i t i v i t y t o i n f l i g h t winds Bnd t u r b u l e n c e . C. T e r r e s t r i a l Environmeht 1. The N a t i o n a l Weather Records Center (GovernmeBt Order 76789) The 1966 Cape Kennedy s e r i a l l y complete winds a l o f t wete r e c e i v e d from t h e H a r i o n a l Weather Records Center. A f t e r accuracy checks, t h e o b s e r v a t i o n s , when &dded t o t h e p r e s e n t d a t a , w i l l i n c r e a s e t h e sample s i z e t o 11 y e a r s . The p e r i o d of r e c o r d of two of t h e primary s t a t i s t i c a l d a t a samples was a l s o i n c r e a s e d by 6 months w i t h t h e a d d i t i o n of January-June 1968, Cape Kennedy h o u r l y peak ground winds, and J u l y December 1967, Cape ~ e n n e d yh o u r l y s u r f a c e o b s e r v a t i o n s . A r e p o r t e n t i t l e d 'iidarkov C h a i ~Techn-Lques f o r P r e d i c t i n g t h e Maximum Wind i n t h e I4aximuitl Dynamic P r e s s u r e Regi0t.t f a 2 Launching Space V e h i c l e s , " by H. L. CrutkHer and N, B. Guttman, prepared under Government Order 76789 w i t h t h e NWRC was r e c e i v e d and submitted f o r p u b l i c a t i o n a s a c o n t r a c t a r r e p o r t . Other NWRC p u b l i c a t i o n s being p r e pared f o r i s s u a n c e a s conPractor r e p o r t s a r e : 2. (a) " P r e d i c t i o n of t h e Maximum Wind Speed i n t h e 10-15 km Layer Above Cape Kennedy," (b ). "Thunders t o r h Pers E s t e n c e a t Cape Kennedy, F l o r i d a (c) "An Empirical Analysis of the 10-15 km Maximum Winds t o Determine Apollo and AAP Launch O p p o r t u n i t i e s Cape Kennedy, F l o r i d a . " ." - Kaman Nuclear (NAS8-11348) Kaman Nuclear p u b l i c a t i o n s being i s s u e d a s c o n t r a c t o r r e p o r t s a r e "The E f f e c t s of Atmospheric F l u c t u a t i o n s and R e p r e s e n t a t i o n Upen Propagated Sound," aRd " V g r l a b i l i t y 6f Sound Propagation red i c t i o n Due t o Atmospheric V a r i a b f l i t y . " �3. Eockheed A Lockheed C o n t r a c t o r Report d e t a i l i n g t h e AS-504 launch p r o b a b i l i t i e s by hour, a s determined by atmospheric c o n s t r a i n t s , was i s s u e d under o f f i c e memorandum R-AERO-YT-10-69, January 29, 1969. V. AEROPHYSICS DIVISION A. Mechanical Design O f f i c e 1. BalanceIModel System f o r Plume Study i n IBFF Design i s n e a r completion on a balance/model system f o r measuring normal f o r c e s on an e i g h t - i n c h s q u a r e f l a t p l a t e d u r i n g a plume impingement t e s t i n t h e IBFF. The system u t i l i z e s t h r e e q u a r t z load washers and can be p i t c h e d t o 30° a n g l e of a t t a c k . (-AD) 2. 5-Component, Micro-Force Balance f o r t h e Low D e n s i t y Chamber Design, d r a f t i n g and drawing check-out has been completed on Balance No. 224 and i t s r e l a t e d c a l i b r a t i o n and i n s t a l l a t i o n equipment. F a b r i c a t i o n w i l l be i n i t i a t e d upon r e q u e s t of t h e o r i g i n a t i n g organization. (-AE) 3. E l e c t r o n Beam Equipment f o r t h e Low Density Chamber F i n a l drawings have been completed on t h e E l e c t r o n Beam Gun designed by D r . B e y l l c h f o r R-AERO-AE. Fabrication w i l l be i n i t i a t e d by d i r e c t c o n t r a c t through P&C, r a t h e r t h a n our u s u a l procedure through ME Laboratory. It i s e s t i m a t e d t h a t 1600 hours w i l l be r e q u i r e d t o f a b r i c a t e t h i s item. The s t a t u s of o t h e r items i n t h i s d e s i g n package a r e (1) E l e c t r o n Beam C o l l e c t o r ( D r a f t i n g ) , (2) E l e c t r o n Beam O p t i c a l Equipment ( ~ ei sg n ) , and (3) E l e c t r o n Beam P o s i t i o n i n g Device (Design) (-AE) . 4. The following i s a p a r t i a l l i s t of p r o j e c t s and t h e i r current status: Cryo-panels, 18' diameter IBFF Vacuum Tank, -AE Design Model Cover, 18' diameter IBFF Vacuum Tank, -AE Des i g n Heated Plenum Chamber, LDC, -AE Design F l a t P l a t e Heat T r a n s f e r Model, LRC 4' WT, -AT Design �P r e s s u r e Model, 2.7'' d i a m e t e r , HRE, -AD Des i g n P r e s s Model, Cone, w i t h Transducers, AEDC WT, -AU Des i g n C a l i b r a t i o n C r o s s , HRE, -qE Dee i g n X-Y-Z P o s i t i o n i n g Devices, L a s e r s , -AF Design M o d i f i c a t i o n Model, No, 397, CFD, -AF $abr i c a t i o n Helium Vent Equipment, 14" WT, -AD Fabrication P r e s s u r e Model, 1 / 4 C y l i n d e r , IBFF, -AE Fabrication Supersonic T e s t Spool, HRE, -AE Fabrication Sonic Nozzle, CFD, -AF Delivered Pos i t i o n i n g Equipment, L a s e r , 7" WT,' -AF Delivered M o d i f i c a t i o n of Plodel No. 422, 14" WT, -AE Delivered C a l i b r a t i o n Equipment, HRE, -AE Delivered Redesigned Survey Probe, 14" WT, -AE Delivered Model 425, Curved C e n t e r l i n e Force Model, 14" WT, -AD Del i y e r e d M o d i f i c a t i o n of Model 392, 14" WT, -AD Delivered Gas H e a t e r , LDC, -AE Delivered O p t i c a l Equipment Support, CFD, -AF Delivered B. Aerodynamic Design Branch 1. Saturn V a. AS-503 Aerodynamic F l i g h t E v a l u a t i o n The f l i g h t compartment p r e s s u r e s compared w e l l w i t h t h e p r e d i c t e d band f o r each compartment on t h e v e h i c l e e x c e p t t h e S-IC b a s e compartment. The p r e s s u r e i n t h i s compartment was lower t h a n pred i c t e d due t o a n i n c r e a s e i n leakage a r e a because t h e f u e l l i n e boots were n o t i n s t a l l e d , �The AS-503 v e h i c l e , a s w i t h p r i o r S a t u r n f l i g h t s , f l e w a t v e r y low a n g l e s of a t t a c k t h a t d i d n o t exceed 2.5 d e g r e e s d u r i n g t h e p e r i o d of i n t e r e s t . Because of t h i s , a r e l i a b l e s t a b i l i t y and f i n l o a d a n a l y s i s could n o t be made, The AS-503 b a s e p r e s s u r e f e l l w i t h i n a p r e d i c t e d band based on AS-502 d a t a even though AS-503 had a 2-degree o u t b o a r d e n g i n e c a n t and o n l y s i x v a l i d b a s e p r e s s u r e measurements,whereas AS-502 had e i g h t measurements. The r e v i s e d b a s e a x i a l f o r c e o b t a i n e d from AS-503 f l i g h t d a t a f o r t h e A p o l l o j S a t u r n V v e h i c l e h a s b e e n p u b l i s h e d i n o f f i c e memo R-AERO-ADV-69-6. The d a t a a r e t o be used i n performance and c o n t r o l studies . b. S a t u r n V S t a t i c Ground Wind Loads R e s u l t s of LTV t e s t LSWT-253 (August 1967) have b e e n compiled f o r b r a n c h r e c o r d i n o f f i c e memorandum R-AERO-AD-68-72, " S t a t i c Ground Wind Loads f o r t h e A p o l l o / ~ a t u r nV Launch V e h i c l e , " by K . L. B l a c k w e l l . These d a t a a r e a v a i l a b l e upon r e q u e s t . 2. S a t u r n V and AAP a. Venting Northrop-Huntsville has published a f i n a l r e p o r t (TR-794-434) c o v e r i n g a n a n a l y s i s of t h e o r i f i c e flow c o e f f i c i e n t d a t a o b t a i n e d i n t h e Ames R e s e a r c h C e n t e r ' s 6 - f o o t S u p e r s o n i c Wind Tunnel. P l a n s a r e made t o do a d d i t i o n a l e x p e r i m e n t a l work which w i l l supplement t h a t of Ames a s w e l l as a d d i t i o n a l work on o r i f i c e s l o c a t e d i n a d v e r s e f l o w f i e l d s . The m a j o r i t y of t h i s work p r o b a b l y w i l l be c a r r i e d o u t i n t h e MSFC 1 4 - i n c h TWT. b. Hydrogen Vent Study (S-IVB Hydrogen Tank) O f f i c e memorandum R-AERO-AD-68-70, " P r e t e s t I n f o r m a t i o n f o r a n I n v e s t i g a t i o n t o Determine t h e Downstream D i s s i p a t i o n of Helium I n j e c t e d from a C i r c u l a r P o r t P e r p e n d i c u l a r t o t h e 1 4 - i n c h TWT Wind Tunnel w a l l , " December 30, 1968, h a s been i s s u e d . Hardware d e s i g n h a s b e e n comp l e ted e x c e p t f o r minor mod i f i c a t i o n s t o t h e o r i g i n a l d e s i g n , and f a b r i c a t i o n i s underway. A c o n f e r e n c e was h e l d w i t h R-AERO-AE and R-AERO-AM t o c o o r d i n a t e hardware and t e s t p r e p a r a t i o n s . T e s t i s s c h e d u l e d f o r March 1960. �3. AAP a. AAP-2 Nose Shroud Venting To reduce t h e a c o u s t i c n o i s e l e v e l on t h e AAP-2 MDA, i t was decided t o s u b s t i t u t e helium i n p l a c e of n i t r o g e n a s t h e gas used t o purge t h e nose shroud compartment. Simultaneously, means of reducing t h e weight of t h e nose shroud (AS-203 t y p e ) by some 400 pounds a r e being investigated. One means of a c h i e v i n g a weight r e d u c t i o n i s t o r a i s e t h e i n t e r n a l p r e s s u r e l e v e l abave t h a t p r e s e n t l y p r e d i c t e d u s i n g a v e n t a r e a of 150 i n 2 w i t h a gaseous n i t r o g e n purge. It t h e r e f o r e becdhles necess a r y t o be a b l e t o a c c u r a t e l y p r e d i c t i n t e r n a l p r e s s u r e l e v e l s when v e n t i n g w i t h helilrm. S i n c e helium i s an extremely l i g h t g a s , i t s p r o p e r t i e s and v e n t i n g c h a r a c t e r i s t i c s a r e s i g n i f i c a n t l y d i f f e r e n t from n i t r o g e n . . T e s t s have r e c e n t l y been conducted a t MSFC t o compare t h e c h d r a c t e r i s t i c s of n i t r o g e n and helium v e n t i n g t o q u i e s c e n t a i r . Tn March f u r t h e r t e s t s i n t h e MSFC 1 4 - i n c h T r i a o n f c blind Tunnel w i l l s i m i l a r l y compare t h e two g a s e s when v e n t i n g i n t o an e x t e r o a l stream. b. AAP-2 S o l a r Array F a i r i n g S e v e r a l ppoblerns have been encountered w i t h t h e pres e n t l y proposed means of v e n t i n g t h e U P - 2 s o l a r a r r a y f a i r i n g d u r i n g f l i g h t (Ref. R-AERO-AD-68-45). The primary problem i s t h a t of keeping the b u r s t load on t h e f a i r i n g t o a minimum s i n c e the f a i r i n g can o n l y be a t t a c h e d on each end t o t h e S-IVB s t a g e forward and a f t s k i r t s . The v e n t l o c a t i o n p r e v i o u s l y s e l e c t e d t o produce a low i n t e r n a l p r e s s u r e i s u n s u i t a b l e f o r p r e - f l i g h t purging, and thus t h e i n - f l i g h t v e n t s must be c l o s e d f o r purging and opened j u s t b e f o r e l i f t - o f f . Clearance problems, however, i n h i b i t t h e use off v a l v e s t o a c h i e v e t h i s , and a c c e s s t o t h e f a i r i n g o p p o s i t e t h e tower p r e v e n t s removing v e n t covers w i t h l a n y a r d s . A 1 t e r n a t e means of v e n t i n g t h e f a i r i n g a r e p r e s e n t l y being i n v e s t i g a t e d . The most a t t r a c t i v e i s t o v e n t o u t t h e b a s e of t h e f a i r i n g where an o r i f i c e w i l l e x i s t f o r t h e purpose of dumping t h e p r e - f l i g h t purge g a s . This v e n t i n g scheme would appear t o be a c c e p t a b l e provided t h e e x t e r n a l p r e s s u r e a t t h e base of t h e f a i r i n g can be a c c u r a t e l y d e f i n e d . c. AAP Plume Impingement (1) A n a l y t i c a l work by LMSC (under m i s s i o n s u p p o r t ) d e f i n i n g WACS plume impingement l o a d s on t h e Workshop s o l a r panels and protuberances has been completed. These d a t a have been developed f o r two-size s o l a r a r r a y s and p a r a m e t r i c a l l y a s a f u n c t i o n of s o l a r panel o r i e n t a t i o n a n g l e . The d a t a a r e being prepared f o r p u b l i c a t i o n . �(2) A s c o p e of work h a s b e e n p r e p a r e d f o r a proposed c o n t r a c t t o d e t e r m i n e s c a l i n g p a r a m e t e r s n e c e s s a r y f o r performing e x p e r i m e n t a l low d e n s i t y plume impingement f o r c e t e s t s . The work t o be performed under t h i s c o n t r a c t is i n s u p p o r t of e x p e r i m e n t a l plume impingement f o r c e t e s t s t o be conducted f o r A p o l l o A p p l i c a t i o n s m i s s i o n s . D e t a i l s of t h e s c o p e of work a r e p r e s e n t e d i n o f f i c e memorandum R-AERO-AD-68-66. ( 3 ) Phase I t e s t s (Ref. R-AERO-AD-68-52) i n t h e MSFC Base Flow F a c i l i t y were completed on F e b r u a r y 3 , 1969. These t e s t s t o determine p i t o t pressure d i s t r i b u t i o n s w i t h i n scaled 5-2 e n g i n e plumes r e q u i r e d l o n g e r t h a n a n t i c i p a t e d . P a r a m e t r i c v a r i a t i o n s i n t h e e x p e r i m e n t a l hardware were n e c e s s a r y t o p r o v i d e s u f f i c i e n t i n f o r m a t i o n f o r a n a l y s i s . A r e p o r t documenting t h e s e d a t a w i t h comparisons between e x p e r i m e n t a l and a n a l y t i c a l plume c a l c u l a t i o n s is i n p r o g r e s s . A Phase I1 s t u d y , t o b e g i n F e b r u a r y 1 9 , 1969, w i l l d e t e r m i n e p r e s s u r e s and h e a t t r a n s f e r r a t e s on a f l a t p l a t e immersed i n t h e s c a l e d 5-2 plume. A memorandum documenting t h e o v e r a l l e x p e r i m e n t a l and a n a l y t i c a l e f f o r t i n s u p p o r t of AAP plume impingement h a s b e e n p u b l i s h e d (R-AERO-A- 69-3). d. Helium Venting (AAP-2 Payload Shroud) R e c e n t l y t h e purge g a s f o r t h e AAP-2 payload s h r o u d compartment was changed from n i t r o g e n t o helium. C u r r e n t compartment v e n t a n a l y s e s a r e based on v e n t d i s c h a r g e c o e f f i c i e n t s which were d e t e r mined e x p e r i m e n t a l l y u s i n g a i r a s t h e d i s c h a r g e g a s . Since i t is not known how t h e u s e of h e l i u m a f f e c t s d i s c h a r g e c o e f f i c i e n t s , t e s t s w i l l be conducted t o d e t e r m i n e h e l i u m d i s c h a r g e c o e f f i c i e n t s i n t h e MSFC 1 4 - i n c h T r i s o n i c Wind Tunnel. T e s t s w i l l be r u n c o n c u r r e n t l y w i t h t h e S-IVB hydrogen t a n k v e n t t e s t s s i n c e t h e equipment i s t h e same e x c e p t f o r v e n t c o n f i g u r a t i o n . A r e q u e s t f o r a new v e n t p l a t e h a s been s u b m i t t e d t o R-AERO-AM f o r u s e d u r i n g t h e March 1, 1969 t e s t s . e. UP-2: S o l a r P a n e l Shroud/APS P r e s s u r e T e s t s T e s t s were conducted i n t h e MSFC 1 4 - i n c h T r i s o n i c Wind Tunnel t o d e t e r m i n e p r e s s u r e d i s t r i b u t i o n s o v e r t h e s o l a r p a n e l shroud and APS u n i t s t o examine t h e i n f l u e n c e of t h e new AAP-2 payload s h r o u d c o n f i g u r a t i o n ( g e n e r a l payload s h a p e ) . Data were o b t a i n e d a t Mach numbers of 0.8, 0 . 9 , 1 . 0 , 1.1, 1 . 2 , 1 . 4 6 and 1.96 f o r a n g l e s of a t t a c k up t o 8 d e g r e e s . A r e p o r t documenting t h e t e s t r e s u l t s i s b e i n g prepared. �f. AAP-2 ( P r e s s u r e T e s t & ) The f o l l o w i n g o f f i c e memoranda have been completed over the p d g t r e p o r t i n g p e r i o d and a r e a v a i l a b l e upon r e q u e s t : (1) Lanel D. G , , 6. 6 . D i l l , "Results from ah I n v e s t i g a t i o n t o DeterMing t h e Local P r e s s u r e s and Load ~ i s t r i b u t i o n sW e r a Proposed Forebddy ~ o n f F g u r & t l o r fi o r t h e AAP-2 Launch Vehicles," R-AEROAD-68-69 (Resul td bf MSFC-TWT-463, August 1968). . (2) ~ l a e k w e l l ,K. L , , "Ah I n v e s t i g a t i o n tct Obtain Local P r e s s u r e ~ i s t t i b u t i o f i sover t h e APS Uhit and S o l a r Panel Shroud ( R e s u l t s of MSFC-TWTof t h e S a t u r n fB/MP-2 Vehicle ," R-AERO-AD-~~-'/~ 397, A p r i l 1968). g. B r b i t a l Aaradya&mFcs AAP O f f i c e tnemdranduh R-AERO-AD-69-1, "Orbithl kerodynaaiic Data f o r t h e U P 1 3 and U P 4 4 ~ i d s i ~ r i sJBnhary ~ " 10, 1969, was! published during t h i s r e p o r t i n g period. It c o n t a i n s o r b i t a l aepodynahic d a t a f o r t h e following two con£ igurkitiona s (1) OV3 w i t h docked CShf and LM/AW - LbrZI~l$f gal&r % f r & y sextended. (1) OMS w i k k ddaked Z=&T and L H ~ A ~ - LMJATM s o l a r a r r a y s n o t extended. h. Cantamination - MP isc charge of waste l i q u i d s d u r i n g s p a c e f l i g h t has a l r e a d y c r e a t e d some contafhinatioh problerlns d u r i n g t h e Apolfo m i s s i o n s . For l o n g e r f l i g h t s of l a r g e o r b l t i n g s p a e e s t a t i o n s , t h e s e problems could become s e r i o u s . There a r e p r i m a r i l y two a r e a s of concern: (1) Cont a m l n a t i o n of t h e atmosphete s u r t o u n d i n g t h e a p a c e s t a t i o n and (2) cont a m i n a t i o n of e x t e r n a l s u r f g c e s of t h e s p a t e s t a t i o n . To o b t a i n some i n p d t f n f o r m a t i o n t h a t i s r e q u i r e d i n the s t u d y of t h i s problem, Lotiisiana S t h t e U n i v e r s i t y has been a s s i g h e d a t a s k to i n v e s t i g a t e t h e c h a r a c t e r is t i c s of f l u i d 9 t h a t a r e i n j e c t e d i n t o a vacuum. This t a s k w i l l be one of S e v e r a l t h a t w i l l be included i n a g r a n t t o LSU. The work t o be performed by LSU i s as follows: Gondvct an experimental i n v e s t i g a t i o n of f l u i d 9 when they a r e i n j e c t e d i n t o d Rear-vacuum through s m a l l o r i f i c e s . Determine Che e i z e , s h a p e , v e l o c i t y , d e n s l t y , and d i r e c t i o n of p a r t i c l e s t h a t form kWe6 ehe f l u i d e a t e r s t h e v%cuurh. Water a t s p a c e c r a f t temperature and p r e s s u r e w i l l be used a s t h e f l u i d d u r i n g t h i s i r m e s t i g a t i o n . O r i f i c e �geometries should s i m u l a t e geometries of v e n t s t h a t w i l l be used f o r waste c o n t r o l d u r i n g Apollo A p p l i c a t i o n s m i s s i o n s . D r . F. M. Donovan, J r . and D r . D. Maples, both members of t h e LSU f a c u l t y , w i l l be t h e i n v e s t i g a t o r s f o r t h i s t a s k . Experimental work w i l l be performed i n vacuum chamber f a c i l i t i e s a t t h e NASA M i s s i s s i p p i T e s t F a c i l i t y . The budget f o r t h i s t a s k is $22,000. M r . ~ u i n t r e l la t NASA Headquarters, who i s t h e c o n t r a c t o f f i c e r f o r t h i s g r a n t , has i n d i c a t e d t h a t paper work should be s u f f i c i e n t l y completed s o t h a t work can b e g i n a t LSU d u r i n g February 1969. 4. General a. Body of Revolution Viscous Cross-Flow I n v e s t i g a t i o n ( P r e s s u r e , Force and Flow V i s u a l i z a t i o n ) Design of t h e 2.70-inch diameter o g i v e - c y l i n d e r model t o be t e s t e d i n t h e High Reynolds Number Equipment has been completed and i s b e i n g d r a f t e d . F a b r i c a t i o n of t h e model is t e n t a t i v e l y scheduled t o be completed i n J u l y w i t h t e s t i n g t o begin i n August 1969. A S a t u r n V model of the same diameter w i l l be f a b r i c a t e d and ready f o r t e s t i n g upon completion of t h e o g i v e - c y l i n d e r t e s t s . S e v e r a l a t t e m p t s have been made t o f a b r i c a t e flow v i s u a l i z a t i o n models u s i n g b l a c k epoxy over a s t e e l s h a f t . R e s u l t s t o d a t e have been unacceptable due t o a i r pockets forming d u r i n g t h e pouring of t h e epoxy. We have been a s s u r e d t h a t t h i s problem can be remedied, and a d d i t i o n a l c a s t i n g s a r e being made by ME Laboratory. Contract negotiations a r e progressing f o r the f a b r i c a t i o n of t h e 4.0-inch diameter model t o be t e s t e d i n t h e LTV 4 - f o o t HSWT. Work on t h e f o r c e d a t a t e s t r e s u l t s has slowed c o n s i d e r a b l y because of t h e l o s s of NSL t e c h n i c a l a i d s u p p o r t . b. Nonlinear L i f t of Bodies of Revolution (Wake Flow Survey) A new scope of work, which covers t h e remaining Phase I1 work and t h e e x t e n s i o n of t h e i n v e s t i g a t i o n t o a s u b s o n i c Mach number, has been completed and forwarded t o t h e Purchasing O f f i c e . Phase I1 c o n s i s t s of a p r e s s u r e r a k e survey of t h e v o r t e x flow f i e l d behind a n ogive-cylinder/frustum-cylinder t e s t model c o n f i g u r a t i o n f o r Mach numbers of 0.8 and 1.96 i n t h e MSFC 14-inch TWT. The program w i l l be f i r m l y scheduled when a c o n t r a c t i s f i n a l i z e d , b u t is now t e n t a t i v e l y s e t f o r May 1969. �r a t i o n of Nigh R e y n ~ l d sNumber Equipment f a b r icaged i n c 1i n a t i o n i cal ibrpted i n urvey probe has been designed and i s now being b e , which w i l l determine Mach number and flow ch @nd yaw planes sirnqltaneously, w i l l b e 14pinch TWT d u r i n g February. which w i l l us when complete Tunnel i n Dal available for i g h Reynolds Number Equipment c a l i b g a t i o n r a k e vey probe is p r e s e n t l y i n d e s i g n . The r a k e , c a l i b r a t e d i n t h e LTV 4 - f o o t High #peed WFnd d u r i n g mid-May 1969. The r a k e would then be calibration topl. . C. Aerophys Ccs Branch Experiment be procured and d s l i v e p e d t q P451;"e i n i c h was f i n a l i z e d Cn Dec@pber 1968. a i l a b l e a t low c o s t and egn now be t h e cryopumping s y s tem i g t h e Lpw Che e f f o r t of a d a p t i n g l i q u i d hydrogen 11 m l p i a t u r e n o a % l e s , instrumented with s t a t i c t u r g gkerwcoupPes, a r e now i n t h e d e e i g n s t a p e a . n f i $ u y a t f o n s p e a i f h d by 8-AEBO-AD, $ r e r e q u i r e d j e t - p l u m impingement program. p o r t s and wal These n o z z l e s i n continuati t i o p s and Brgwhnge b v e been completed on t h e and s e n t t o R-L$EPO-RM f o r c o n t r a c t i n t t i a t i o n . eliura c r y o p w p i n g t o the low d e n s t t y wind t u n n e l , i l i t y ts flow n i t r o g e n gas from whish one can e r ~ t u r eby use of a h i g h r e s o l u t i o n s p e c t r o m e t e r . t i ~ ns p e c t r o m e t e r has been ordered f o r use i n CS, Alga, a Q-5000 mass spectrqmete;c has t plume s t u d i e e With t h e addf there e x i s t s measure r o t a t A two-me t e r . i S p e c i f i p a g i o ~ shave been completed on a l i q u i d n i t r o g e n shroud wiCh b l a c k i t e r i o r s u r f a c e s f ~ t rh e low d e n s i t y wind t u n n e l and s e n t t o R-AERO-& for i n i t i ~ t i o n . Fb An e x p e t i m e n t a l cryopanel c o n s i s t + n g of expended honeycomb w a s t e s t e d for t h e IBFP i n t h e Low Density Chamber. Thermocouples were a t t a c h e d , a n d t h e panel was connecged t o t h e l i q u i d n i t r o g e n (LN2) s u p p l y l i n e s i n the Low W p s i t y Chamber. The panel w a s then t e s t e d under vacuum c o n d i t i o n @ t o determine t f a w i e n t cool-down times and t o observe s t e a d y - s t a t e temperature g r a d i e n t s from t h e LN2 s u p p l y l i n e s �t o t h e edge of t h e honeycomb " f i n s . " An a d d i t i o n a l purpose of t h e t e s t s was t o determine what e f f e c t r a p i d temperature c y c l i n g might have on t h e s t r u c t u r a l i n t e g r i t y of t h e aluminum-filled epoxy bond. The expanded honeycomb c e l l s were bonded t o a 0.125-inch machined aluminum p l a t e t o form t h e cryopanel. The t e s t s were cons i d e r e d s u c c e s s f u l from t h e s t a n d p o i n t of t r a n s i e n t cool-down time and s t r u c t u r a l i n t e g r i t y of t h e epoxy bond. Except f o r some poor thermocouple c o n n e c t i o n s , t h e observed temperature g r a d i e n t s from t h e LN2 s u p p l y l i n e s (welded t o t h e cryopanel b a c k s i d e s ) t o t h e f a r t h e s t edge of t h e honeycomb " f i n s " were s t i l l w i t h i n a c c e p t a b l e l i m i t s f o r use i n t h e Impulse Base Flow F a c i l i t y (IBFF). 2. Impulse Base Flow F a c i l i t y A s i z e a b l e q u a n t i t y of d a t a has been c o l l e c t e d from t h e impact p r e s s u r e probe survey of t h e s c a l e d 5-2 engine plume. Impact p r e s s u r e v e r s u s s t a g n a t i o n p r e s s u r e d a t a were c o l l e c t e d a t v a r i o u s s t a t i o n s i n b o t h t h e a x i a l and r a d i a l p l a n e s . Data were c o l l e c t e d t o e v a l u a t e any d i f f e r e n c e s caused by s c a l i n g , combustion chamber O/F g r a d i e n t s , and O / F v a r i a t i o n s due t o v a r y i n g mass flows, and t h e d a t a a r e p r e s e n t l y being compared t o t h e t h e o r e t i c a l plume c o n f i g u r a t i o n . The experimental i n v e s t i g a t i o n i s c o n t i n u i n g w i t h t h e f l a t p l a t e p r e s s u r e impingement s u r v e y scheduled t o b e g i n February 3, 1969. Design of t h e cryopanel s y s tem i s p r o g r e s s i n g s a t i s f a c t o r i l y . S p e c i f i c a t i o n s f o r a l l a s s o c i a t e d hardware a r e 90 p e r c e n t comp l e t e . R-ME i s i n v e s t i g a t i n g some new bonding techniques f o r a t t a c h i n g t h e honeycomb m a t e r i a l t o t h e cryogenic f l u i d l i n e s . 3. High Reynolds Number Equipment F i n a l assembly of t h e High Reynolds Number Equipment has been delayed due t o t e s t s e c t i o n d e l i v e r y s l i p p a g e of 2 months. The f i r s t s h o t i s now scheduled f o r A p r i l 1, 1969. A l l welding has been completed e x c e p t one seam a t t h e d i f f u s e r elbow. This seam r e q u i r e s f i n a l alignment of t h e t u n n e l which is pending d e l i v e r y of t h e s u p e r s o n i c t e s t s e c t i o c o r s p o o l p i e c e t o r e p l a c e t h e t e s t s e c t i o n . D e l i v e r y of t h e s p o o l p i e c e i s expected February 1 0 , 1969. The s u p p l y tube c l e a n i n g , which i s approximately 50 p e r c e n t complete, should be completed by February 1 9 , 1969. C a l i b r a t i o n s c h e d u l e s a r e being made w i t h t h e f i r s t t e s t s i n t h e t u n n e l t o use a 33--static-probe r a k e . The f i r s t c a l i b r a t i o n w i l l be t h e s u b s o n i c Mach number d i s t r i b u t i o n w i t h i n the t e s t s e c t i o n . �T r a n s o n i c c a l i b r a t i o p w i l l probably f o l l o w t h e s u b s o n i c c a l i b r a t i o n provided t h e p r e s e n t d e l i v e r y s c h e d u l e of t h e t r a n s o n i c t e s t s e c t i o n i s maintained, 4. Thermal Acouetic J e t F a c i l i t y The checkout pf t h e helium h e a t e r is a t a s t a n d s t i l l . Fuel e n g i n e e r i n g p p r s a n n e l a r e c u r r e n t l y a t t h e home p l a n t r e p a i r i n g a v a r i a b l e t r a n s f o r m e r t h a t burned because of a broken carbon brush. New, h a r d e r m a t e r i a l w i l l b e used t o ~ e p l a c et h e brushes. FFCO w i l l t r u c k t h e t r a n s former t o HuntavilZe aboug February 1, 1969, and t h e checkout should c o n t i n u e then. The c o n t r a c t o r has ino t a l l e d a redesigned s t i l l i n g chamber which he f e e l s w j l l a l l e v e a t e t h e temperature f l u c t u a t i o n s i n t h e flaw. Nonuniform heatiQg of t h e storbag9 nlatrix d u r i n g t h e h e a t i n g c y c l e i s b e l i e v e d t o be capeing t h e p r ~ b i @ m ~f t h e o u t p u t a i r temperature being s o much l w e r t h a n t h e s t o r a g e pehperature. Only one p s r t f s n a£ t h e m a t r i x is a t t h e h i g h temperature and t h e surroundfng m a t e r l a l a t a much lower temperature. During c a l i b r a t i o n r u n s , t h e incoming a i r i s heated o n l y t o t h e lower tempergture. It is b e l i e v e d t h a t b e t t e r c i r c u l a t i o n o r a g i t a t i o n of phe a i r d u r i n g t h e h e a t i n g c y c l e w i l l s o l v e t h i s problem. A new c r o s s - h e m framework bas been i n s t a l l e d i n t h e Cold Flow Duct f o r t h e fnrthcowingig TITRT EeqEs. 5. 7 x 7 - i n c h B i - s o n i c Wind Tunnel A t e s t was conducted by Wyle L a b p r a t o r i e s f o r R-AERO-AU a s a p a r t of t h e experimental program f o r i n v e s t i g a t i o n of shock t u r bulence i n t e r a c t i o n phenomena. The experiment was performed t o examine t h e p r o d u c t i o n of a c o u s t i e waves i n t h e i n t e r a c t i o n of a shock wave and a t u r b u l e n c e environment. The remaining t u n n e l time was absorbed by the c o n t i n u i n g cross-beam i n v e s t i g a t i o n being performed by R-AERO-AF. 6. 1 4 x 14-inch T r i s o n i c Wind Tunnel The f o l l o w i n g i n v e s t i g a t i o n s were conducted d u r i n g December 1968 and January 1969: (1) A con tinued i n v e s t i g a t i o n by R-AERO-AD t o supplement d a t a from a n e a r l i e r Cest which wqs a n i n v e s t i g a t i o n t o determine l o c a l normal f o r c e g r a d i e p t s on cone-cylinder b o d i e s i n s u p e r s o n i c flow a t low a n g l e s of a t t w k . T o t a l runs: SO. �( 2 ) A c o n t i n u a t i o n by R-AERO-AD of a t e s t t o determine t h e cause of c e r t a i n d a t a i n c o n s i s t e n c i e s i n t h e previous phase. The o r i g i n a l i n v e s t i g a t i o n was t o determine what e f f e c t s t h e removal of t h e i n t e r s t a g e e x t e r n a l coverings could have on the aerodynamic c h a r a c t e r i s t i c s The d a t a d i s c r e p a n c y was due t o a model of a S a t u r n V c o n f i g u r a t i o n . r o l l misalignment caused by e x t e r n a l model p r o t u b e r a n c e s . The problem was c o r r e c t e d and a l l d a t a correlate'd. T o t a l runs: 143. ( 3 ) An i n v e s t i g a t i o n by R-AERO-AD t o determine t h e load d i s t r i b u t i o n a l o n g t h e s o l a r panel shroud and APS u n i t on t h e u p r a t e d AAP/Saturn I B payload c o n f i g u r a t i o n . T o t a l runs: 16. ( 4 ) A continued i n v e s t i g a t i o n by R-AERO-AD i n t o t h e a e r o dynamic p r o p e r t i e s of i n t e r s t a g e r i n g s . The t e s t was conducted t o v e r i f y previous t e s t d a t a and o b t a i n a d d i t i o n a l information. T o t a l runs: 82. (5) An i n v e s t i g a t i o n by R-AERO-AD t o determine t h e flow a n g u l a r i t y i n t h e t u n n e l a t s e l e c t e d s t a t i o n s . This i n v e s t i g a t i o n , which is p r e p a r a t o r y t o a wake s u r v e y t e s t , w i l l a i d i n a c c u r a t e c o r r e l a t i o n of d a t a . 7. Data Reduction Besides the r o u t i n e f a c i l i t y d a t a r e d u c t i o n , t h e programs f o r t h e IBFF were f i n i s h e d , checked o u t , and documented i n a Branch memo. Problems i n t h e program f o r D r . B e y l i c h , r e g a r d i n g t h e o r e t i c a l gas dynamics, were f i n a l l y c l e a r e d up and t h e MARVESS numerical i n t e g r a t i o n techniques worked w e l l . 8. Instrumentation a. High Response Balance The shock t u n n e l b a l a n c e , which was t o be used f o r f o r c e measurements on a f l a t p l a t e a s p a r t of t h e j e t plume s t u d i e s , was reworked and checked o u t . The low range of f o r c e s , t y p i c a l l y l e s s It was f i n a l l y than one pound, p r e s e n t e d c a l i b r a t i o n d i f f i c u l t i e s . resolved t h a t the l i n e a r i t y w a s s u f f i c i e n t t o c a l i b r a t e a t higher l e v e l s and i n c r e a s e t h e g a i n a f t e r t h e c a l i b r a t i o n . b. Crossed-Beam Support The f i e l d t e s t i n g of t h e m u l t i - d e t e c t o r f a n f o r t h e atmospheric crossed-beam program has been moved t o t h e v i c i n i t y of t h e R-AERO-Y f a c i l i t i e s . An i n s t r u m e n t a t i o n van, h e a t e d , a i r c o n d i t i o n e d , and c o n t a i n i n g power r e g u l a t i o n equipment and equipment r a c k s , has been borrowed from R-TEST. Three e x c e l l e n t t a p e r e c o r d e r s were a l s o i n c l u d e d . �D. Thermal Environment 1. ranch Continuum Heating and Mission Support Modeling of t h e S a t u r n AS-501 v e h i c l e f o r t h e purpoBe of c a l c u l a t i n g deafi-body h e a t i n g rates? and s k i n temperatures w i n g t h e ~ o c k h e e dSNORE-CATCH computbr prd$r&m was completed. Temperatures o b t a i n e d were cdmparcd t o t h o s e meadured 6& t h e i n n e r s k i n of t l i k I n s t r u m e n t U n i t . The c a l c b l a t e d teniperattires were approxiniately 15' lower t h a n thoge measured. Thk ef f e k t s a f a n g l e of a t t d c k a t e being added t o t h e model. $hese e f f e k t s w i l l i n c r e d s e the c a l c u l a t e d t e h p e r a t u r e s . Heatihg r a t e s and temperatbres recorded dn t h e f o r d a r d s # i k t , LH2 tank and i n t e k g t a g e of tHe 9-11 s t a g e w i l l a l s o be conipared t b r e s u l t s o b t a i n e d w i t h t h e SHORE-CA$CH p+agrefm. wdkk has begun 6i-1 thk? niotlelitig of t h e AS-203 v e h i b l e f o r the pdrpoge ti£ c $ l c u l a t i n g o t b i t a l h e a t i n g r a k e s tising ti-ie ~ B h k h e e dHe&t Rdhe c m p h t b r program. ~ & t u l t w b i l l be cdhpared t o f l i g h k d a t a t o v e r i f y t h e akWraey of t h e Heat Rate prograta. he s&OF&-CATCH computer Ptdgram mod i f i c a t i6ns a r e being checked o u t . THese fnodifibati6hS included added f l e x i b i l i t y i n i h p u t t i n g p r e s s u r e d a t a and t h e c a p d b i l i t y t U c a l c u l a t e h e a t r a t e s i t i t h e s l i p flow regime. P r e l i m i n a r y & f f d P t s have beeti made t o o b t a i n ebmputer g e n e r a t e d p l o t s fr6m t h e S ~ ~ R E - C B prograin, TC~ Attempts were d d e t o coBvert t h e Beat Rate p+ogram t o t h e 1108 EXEC V I I I dystem. ~ f d c U s & i & i s& r e b@ing h e l d t o e d r r e c t t h e e r r o r s caused by i r i c a r r e c t cdnipilatioa bf the prdgkam. 2. Mission Supputt a. Shear Laybrs The r e a l i s t i c p r e d i c t i o n of cofiditions p r e s e n t a t tHe i n j e c t o r f a c e has been s t u d i e d . These p r o p e r t i e s a r e n e c e s s a r y f o r i n p u t i n t o t h e mixing progkams used t o a n a l y z e t h e combuStion chamber. For s m a l l l i q u i d - p r o p e l l a t i ? e n g i n e s , t h e e f f k c t of d r o p l e t s i n t r o d u c e s a n a d d i t i o r f a l l o s s i n t h e combustion prdkeks. D r o p l e t v a p o r i z a t i o n models a r e b e i n g c o l l e c t e d . ~ a l c d l a t i d r iof mixing e f f e c t s i n t h e R ~ D cofibustion chamber, excluding d r o p l e t s , has been s t a r t e d . b. Nozzle and J e t Wake A f t e r t h e s t u d y of t h e R4D r o c k e t motor flow f i e l d was completed, i t wag discovered t h a t t h e m i x t u r e r a t i o d i s t r i b u t i o n Currently, e f f d r ts a r e underway t o o b t a i n documentation f o t the c o r r e c t d is t r i b u tFdh and then t o r e - r u n tHb c a l c u l a t i d h using t h e c o r r e c t e d O/F g r a d f e n t . The c a l c u l a t i o n S w i l l t h e n be compared w i t h t h e r e c e n t t e s t d a t a obtait-iod from MSC. was s u b s t a n t i a l l y d i f f e r g n t from t h e d i s t r i b u t i o n analyzed. �Work i s being conducted t o e s t a b l i s h a u s a b l e condensat i o n model f o r multi-component vapor expansion. The g r e a t e s t amount of experimental t h e o r e t i c a l work done on condensation of expanding g a s e s has been concerned w i t h pure v a p o r s . For r e a l i s t i c a p p l i c a t i o n s , an e n g i n e e r must determine the e f f e c t s of condensation i n a m u l t i - s p e c i e s vapor. M o d i f i c a t i o n s of e x i s t i n g pure vapor t h e o r i e s a r e being i n v e s t i g a t e d and used t o p r e d i c t t h e e f f e c t s of condensation i n a multi-component expanding flow. 3. Laser Velocimeter S t u d i e s A l a s e r doppler v e l o c i m e t e r has been developed which is capable of making v e l o c i t y and t u r b u l e n c e measurements on a gaseous flow. Data o b t a i n e d from measurements on a s u b s o n i c j e t have shown good promise. Comparisons between t u r b u l e n c e i n t e n s i t y and t u r b u l e n c e s p e c t r a l power d e n s i t y measurements from b o t h t h e v e l o c i m e t e r technique and the h o t w i r e anemometer method gave s a t i s f a c t o r y agreement. F u r t h e r experiments on a s u b s o n i c j e t a r e planned i n t h e l i g h t of t h e e x p e r i e n c e gained w i t h t h e f i r s t s e t of measurements. Subsequent a p p l i c a t i o n s w i l l b e t o measurements of t h e mixing r e g i o n of a s u b s o n i c j e t and flows around h i g h a n g l e - o f - a t t a c k aerodynamic p r o f i l e s . A C 0 2 l a s e r doppler v e l o c i m e t e r is being developed f o r atmospheric a p p l i c a t i o n s . A system i s being b u i l t capable of a twometer s p a t i a l r e s o l u t i o n a t 150 meters which w i l l be used t o s t u d y t h e v e r t i c a l wind v e l o c i t y p r o f i l e near t h e e a r t h ' s s u r f a c e . Subsequent a p p l i c a t i o n s a r e t h e s t u d y of t r a i l i n g v o r t i c e s g e n e r a t e d by a i r c r a f t and t h e long range d e t e c t i o n of c l e a r a i r t u r b u l e n c e . 4. O p t i c a l Measurements of Plumes A cold flow t e s t was conducted a t AEDC w i t h a l a s e r d o p p l e r v e l o c i t y i n s t r u m e n t ( v e l o c i m e t e r ) t o determine t h e v e l o c i t y f i e l d i n t h e b a s e and e x h a u s t r e g i o n s of a four-nozzle model of t h e S a t u r n I1 type. The t e s t was t h e f i r s t e f f o r t t o use t h e v e l o c i m e t e r i n a low d e n s i t y s u p e r s o n i c flow. An e q u a l l y important purpose of t h e t e s t was t o e v a l u a t e t h e v e l o c i m e t e r and v e l o c i m e t e r s u p p o r t systems ( e l e c t r o n i c and contaminant systems) a s an i n t e g r a t e d system. While t h e week of t e s t i n g d i d n o t produce t h e v e l o c i t y f i e l d , t h e s y s tem "shakedown" has provided an important b a s i s f o r i n s t r u m e n t changes t h a t should extend t h e instrument range t o i n c l u d e flow f i e l d s o f t h e type encountered i n t h e t e s t . Those changes a r e c u r r e n t l y being e v a l u a t e d i n response t o a r e - e n t r y of t h e cold flow t e s t t e n t a t i v e l y scheduled f o r September 1970. I n a d d i t i o n , r e f i n e ments a r e b e i n g considered t o upgrade the r e l i a b i l i t y of the v e l o c i meter s u p p o r t system. A l l of t h e instrument and instrument s u p p o r t system d e f i c i e n c i e s a r e being e v a l u a t e d i n p r e p a r a t i o n f o r t h e 1970 t e s t entry. �5. Plume fmpingement Heating & e a t i n g ratee t o v a r i o u s components on the ~ a t u r n l A Acon~ f i g u r a t i o n due t o plume impingement a r e b e i n 8 c a l c u l a t e d . S p e c i f i c a r e a s b e i n g Cohsidered are (1) h p i n g e ~ e n ts f W/RCS engine on MDA r b d i a t i o ~ , q (2) i i - i n g e i n e n t of WJRCQ kngiIIed 6a Solded ATM s o l a r p a n e l s , (3) impingeinent of ESMJRCB engfiies ori MDr$ forwbrd cone, and (4) impingement of cSM/ RCS engines on unfolded Am s o l a r p a n e l s . The a n a l y s i s of ebe f i r s t t h r e e a r e a s i s ebmplete and is being d o c w n t e d . The fourth. a r e a has been analyzed Bed pre1j;mlmry r e s u l t s have been o b t a i n e d . !Phis p r e l iminary arlalyO is $8 p r e s e n t l y being *ef i n e d , The Egret: I3yfFrirplizaLig-n ~ e & t p i u ; l ~a ~aumeficsal m t h a d t o o b t a i h t h e 5hI@@otao 8BlQtioit Q& & iskt a5 p a r t i a l dLEEer@ntfal equatioHs, has sa@ee$8ful hy salved t h e Pdoai pa$ t r a n s o h l g f l~ problem. The method has d-ngtrdted i t &$ b i l i t y t e fiad smooth and ~e.11-behaved flow f i e l d solyk%oi%$ Pn hoaile @siBtltguus~ 5 t ha v a r y sm.zill ithpoat raddus of c u r v a t u r e . Th%sW r k has bee& d 6 c m e a t e d i n Lockheed dDkswment TM 541 20-213, ~ s G / & U ~ C B~a46622~ '"A $ & ~ f i s o n i cN ~ i a l eS o l u t i o n the E r r o r MTQimFzation ~ e e h n i q u e , 'bp ~ R, J, B~D$FABJ .dind D. E. Ko.ok@t, J&naasy 1969. F u t u r e plans ckll fi6r Bncok@or.ihk$LqkAs ief Eects -sf equi'i$be&umJf rozen r e a c t i n g g a s m t z t u r c $ and f u e l ~ t & $ & t ~ i e (OJF n S g ~ a d i e n a )i n t o t h e praeenk t r a n g d n i c nbsele siolkitbh. The c a l c u l a t i p n of %he e 1 e c t r - e ~ d e n s i t y d i s t r i b u t i o n i n t h e 5 n v I s c i d plume and the S h a r layer QZ tb6 Z"I e e h e exha@t plume a t 10,'04)0 f e e t a l t i t d e has been ,eMpl.eted, The Aero-Cbem ~ ~ y k e c iStreamd lcme 'P'rograni bad bee^ mod h g b d to faei.1 & a t e bts u s e by witking ~ m u n $ c a eion of d a t a from the f l o e f i e l d grograms d i r e c t and automatkc. The c a p a b i l i t y t o restarc t h e &alcukbrtLon a16Dg .a s t r e a m l i n e has been added to p r o v i d e a n a c c u r a t e me-t:b'od t o compu.te entire nozzle l e n g t h w i t h o u t r e g u i r ing excess i v e b l o c k s @f Icorgputer r u n tidies . he BASAI Lewii$, k h e m . ~ c h e m j m lanalys i s i.n bas f c f o m u l a t i o n Is s h i t e d !to p r e d i c t Dhe d e g r e e of ioni.uation and hence s h e e l e c t r o n mole d e h ~ S k yWE a gaseous tays tern a t e q u i l Zbriumn, U n f o r t u n a t e l y , S T E ~ E ~ ~ ?of ~IS i o n $ ~ e dS p e c i e s and Eree,e;lecCrons a r e s o s m a l l , from a the~moChem5ca.l :p.Oint of v . W , chat tL&, A $ A / ~ e w i sprogram i s n u m e r i c a l l y aneaiired ,t,o p e r F ~ r mt h e cailcul&~tian. A supplemental t e c b n t q u e has been pr&gramed t.o p e r f o r m "this ~ a l c u ; L : ~ t i Th5s ~ n ~ !program, which is b e i n g che*ed ouZ, r e q - u b e s ou%ptit fr a n t h e ~ U A l ~ e w ic sa l c u l a t i ~ nas .input. �8, Vacuum ~ G ~ ai o n ns Study The purpose of t h i s i n v e s t i g a t i o n i s t o develop a mathem a t i c a l technique f o r t h e d e s c r i p t i o n of t h e h i g h a l t i t u d e and s p a c e An experimental environment expansion of an axisymme t r i c gaseous j e t . program w i l l be conducted t o provide experimental d a t a f o r comparison with a n a l y t i c a l predictions. A s e t of p a r t i a l d i f f e r e n t i a l e q u a t i o n s which d e f i n e t h e v e l o c i t y , d e n s i t y and s t r e s s t e n s i o n i n t h e flow f i e l d has been d e r i v e d . This d e r i v a t i o n was made f o r a s i n g l e component, monatomic g a s , u s i n g t h e B-G-K approximation f o r t h e c o l l i s i o n i n t e g r a l . M e t h o d - o f - c h a r a c t e r i s t i c s s o l u t i o n s t o t h i s s e t of equat i o n s have been developed f o r t h e c a s e s of n e g l i g i b l e and non-neglig i b l e s h e a r s t r e s s . These s o l u t i o n s a r e c u r r e n t l y being programmed. Using t h e m e t h o d - o f - c h a r a c t e r i s t i c s e q u a t i o n s , r e p o r t e d i n t h e previous p r o g r e s s r e p o r t , a s e t of e q u a t i o n s was obtained f o r d e s c r i b i n g t h e flow around a c o r n e r expansion, s u c h a s a n o z z l e l i p . A computer program has been developed f o r a m e t h o d - o f - c h a r a c t e r i s t i c s nozzle plume flow f i e l d , i n c l u d i n g t h e corner expansion. This program i s being checked o u t . 9. Study of Dual Channel Spectroradiometer An i n t e r i m r e p o r t (Rocketdyne Report R-7733) d e s c r i b i n g t h e d a t a o b t a i n e d under Phase I1 of t h e c o n t r a c t has been r e c e i v e d . S p e c t r a l d a t a and zone r a d i o m e t r y d a t a were obtained a t t h e e x i t p l a n e of a b e l l n o z z l e f o r f i v e d i f f e r e n t p r o p e l l e n t combinations. These d a t a , however, were n o t s u f f i c i e n t t o determine temperature and s p e c i e p a r t i a l pressure p r o f i l e s . The s p e c t r o r a d i o m e t e r i s now being modified t o a l l o w f a s t e r s c a n r a t e s and w i l l be used t o o b t a i n a d d i t i o n a l d a t a on f i r i n g s t o be conducted i n March. E. Unsteady Gas Dynamics Branch 1. I n f l i g h t Acoustic a . Data r e d u c t i o n a n a l y s i s has begun on t h e AEDC 4 p e r c e n t model s u p e r s o n i c d a t a . C u r r e n t l y , o v e r a l l l e v e l s s c a l e d t o f u l l s c a l e c o n d i t i o n s a r e being computed and p l o t t e d . Cross spectrum a n a l y s i s has begun. b. The experimental p o r t i o n of t h e shock t u r b u l e n c e i n t e r a c t i o n s t u d i e s has been completed. The d a t a a r e being reduced. - �c. A d d i t i o n a l c o n t r a c t work f o r t h e "Development of F u l l P n f l i g h t A c o u s t i c Design C r i t e r i a S c a l i n g E f f e c t s " has been i n i t i a t e d . Data from AMES' f o u r p e r c e n t S a t u r n V, PSTL-1 and PSTL-2 wind t u n n e l t e s t c o n d i t i o n s and f l i g h t w i l l be used. A l l o t h e r d a t a a v a i l a b l e i n t h e l i t e t a t u r e w i l l be included. p r e l i m i n a r y d a t a r e d u c t i o n is continuing. d. A wind tclnnel prograth has been conducted i n t h e AEDC 1 6 - f o o t t r a n s o n i c t u n n e l t o provide experimental i n f o r m a t i o n t o h e l p d e r i v e methods by which f l u c t u a t i n g a i r l o a d s i n t h e r e g i o n a£ prohis wind tuberances can be a c c u r a t e l y p r e d i c t e d on launch v e h i c l e s . t u n n e l t e s t program is i n s u p p o r t of a c d d k r a c t w i t h Wyle L a b o r a t o r i e s , H u n t s v i l l e , Alabama e n t i t l e d "En%irbnment Around ProtubBtances SubS t a t i c p r e s s u r e d a t a have been analyzed merged i n a Boclndairjir Layer.'' afid t h e pkelimihqk$ & e d u c t i o n bf the f l u c t h a t i n g p r e s s u r e d a t a iS i n pragres8, e. A j o i n t MSFc/Air Fotce wirld t u n n e l t e s t plPogram has been conducted. his t e s t program c o n ~ i s t e dof s e v e r a l becofiic hose c o n f i g u r a t i o n s which w i l l provide a b a s i s f o r a n a l y s e s of t h e c r o s s c o r r e l a t i o n c h a r a c t e r i s t i c s ( a e e e s s a r y f o r d e s i g n c r i t e r i a ) of t h e i n f l i g h t f l u c t u a t i n g p r e s s u r e e n v i r o m e n t f o r v a r i o u s AAP mibsions. U P d e s i g n s p e c i f i e r t t i o n s a r e e t t r r e n t l y being d e r i v e d frbm t h e s e d a t a . The i n i t i a l s p e c i f i c a t i o n s f o r U P - 2 and 4 w i l l i n c l u d e o v a f a l l l e v e l s v e r s u s body s t a t i o n , 2. ~ a u n c hS i t e Acd.ustics a. A c t i v i t y a t t h e Acoustic Model T e s t F a c i l i t y (AMTF) a t T e s t L a b o r a t o r y has slowed d u r i a g t h e p$st mbnth. Plans a r e now being i n i t i a t e d t o conduct a 20 percetlt S a t u r n V model r o c k e t n o i e e e x p e r i ment. This experiment has been desighed t o o b t a i n amplitude and phase ifiform8tion f o r b o t h t h e launch and s t a t i c f i r i n g c o n d i t i o n of t h e S a t u r n V v e h i c l e . S p e c t r d l and s p a t i a l c o r r e l a t i o n c h a r a c t e r i s t i c s w i l l be o b t a i n e d f o r a v e h i c l e a s w e l l as t h e immediate launch cunplex , area . b. The s t u d y of ground a t t e n u a t i o n e f f e c t s on a c o u s t i c wav6 p r o p a g a t i o n i s c o n t i n u i n g w i t h more d e t a i l e d a n a l y s i s being g i v e n t o t h e m e t e o r o l o g i c a l parameters. A & r e a p p l i c a b l e model i n terms of t h e p h y s i c a l phenomena i s being sought f o r p r e d i c t i o n a c c u r a c y a p p l i c a t i a n of t h e r e s u l t s . ' �3. Panel F l u t t e r a . The upcoming h i g h a l t i t u d e S a t u r n V S-IVB p a n e l f l u t t e r t e s t , o r i g i n a l l y s c h e d u l e d t o e n t e r t h e ARC 2 x 2 - f o o t t r a n s o n i c wind t u n n e l i n F e b r u a r y 1969, has been d e l a y e d b e c a u s e t h e n o n c o n t a c t i n g d i s p l a c e m e n t m e t e r s were n o t o b t a i n e d on s c h e d u l e . To d a t e , t h e o n l y company t o respond t o a n RFQ f o r t h e s e m e t e r s i s t h e Wayne-Kerr Corporat i o n of G r e a t B r i t a i n . T h i s , of c o u r s e , has caused problems due t o t h e "Buy American Act" c o n t a i n e d i n t h e C o n t r a c t (NAS8-21250). These m e t e r s a r e r e q u i r e d f o r v i b r a t i o n t e s t s b e f o r e t h e wind t u n n e l t e s t , as w e l l as f o r t h e wind t u n n e l t e s t i t s e l f . T h e r e f o r e , t h i s d e l a y h a s postponed t h e t u n n e l e n t r y d a t e u n t i l a t l e a s t May 1969. No problems have been e n c o u n t e r e d f o r t h e r e s t of t h e g o v e r n m e n t - f u r n i s h e d equipment r e q u i r e d f o r t h i s c o n t r a c t . The boundary l a y e r r a k e r e q u i r e d h a s been f a b r i c a t e d and w i l l be s h i p p e d t o McDonnell w i t h i n t h e n e x t few d a y s , b . The roughened s o l i d s i d e w a l l boundary l a y e r p r o f i l e i n v e s t i g a t i o n , conducted i n t h e MSFC 1 4 x 1 4 - i n c h t r i s o n i c wind t u n n e l i n s u p p o r t o f t h e above mentioned p a n e l f l u t t e r t e s t , h a s y i e l d e d good r e s u l t s . A memorandum i s b e i n g p r e p a r e d t o d e s c r i b e t h e t e s t and present the data. c . S t u d i e s t o d e t e r m i n e t h e l i m i t c y c l e b e h a v i o r of f l u t t e r i n g clamped p l a t e s , t a k i n g i n t o a c c o u n t t h e e f f e c t s of i n - p l a n e compress i v e l o a d s , d i f f e r e n t i a l p r e s s u r e l o a d i n g s and c a v i t y , a r e b e i n g continued. The computer program, developed by P r o f e s s o r E a r l H. Dowell and P r o f e s s o r Voss a t P r i n c e t o n U n i v e r s i t y , was m o d i f i e d t o c a l c u l a t e (1) f u l l l i n e a r i z e d aerodynamic f o r c e s , ( 2 ) f l u t t e r r e s p o n s e u s i n g t h e computed aerodynamic f o r c e , and ( 3 ) s t r e s s e s i n p a n e l due t o i t s f l u t t e r deformation. 4. Ground Winds A d d i t i o n a l S a t u r n V wind t u n n e l t e s t d a t a have b e e n f u l l y reduced u s i n g t h e Lockheed and Boeing d a t a a n a l y s i s programs. E f f o r t s a r e underway t o u s e t h i s newly reduced d a t a i n b e t t e r d e f i n i n g S a t u r n V f u l l - s c a l e l o a d p r e d i c t i o n s f o r a l l b a s i c on-pad w e i g h t c o n f i g u r a t i o n s w i t h and w i t h o u t t h e MSS, and w i t h and w i t h o u t t h e damper a t t a c h e d (where a p p l i c a b l e ) . A p r e l i m i n a r y i n v e s t i g a t i o n h a s b e e n conducted i n r e d u c i n g ground winds w i n d - t u n n e l t e s t d a t a by means of a n a n a l o g s y s tem. The method a p p e a r s f e a s i b l e and t h e b a s i c a n a l o g c i r c u i t h a s b e e n �o u t l i n e d f o r t h e d a t a r e d u c t i o n system. Design and c o n s t r u c t i o n of t h e analog system w i l l be completed when funds a r e approved. Load p r e d i c t i o n s were made f o r the most c r i t i c a l wind a z i muths of t h e S a t u r n V AS-503 v e h i c l e c o n f i g u r a t i o n s d u r i n g launch coyntdown f o r s e v e r a l wind p r o f i l e s f o r m o n i t o r s h i p of AS-503 CDDT and launch countdown. This type of wind load p r e d i c t i o n s i s being extended f o r more c r i t i c a l wind azimuths and weight c o n f i g u r a t i o n s f o r AS-504 and subsequent v e h i c l e s , A s t u d y t o determine second mode e f f e c t s on ground wind l o a d i n g s f o r t h e S a t u r n V v e h i c l e i s s t i l l i n p r o g r e s s . Also, a prel i m i n a r y s t u d y has been conducted t o determine t h e e f f e c t s on graund wind load p r e d i c t i o n s r e s u l t i n g from measuring wind v e l o c i t i e s a t t h e 445-foot EUT l e v e l r a t h e r t h a n t h e 60-foot l e v e l . VI. ASTRODYNAMfCS AUD GUIDAEJCE THEDRY DIVISION A. O p t i m i z a t i o n Theory Branch 1. Lunar Roving Vehicle S t u d i e s P r o p o s a l s submitted i n response t o t h e c e n t e r ' s RFQ f o r phase B s t u d i e s of a d u a l mods l u n a r roving v e h i c l e (DLRV) were e v a l u a t e d and recommendations were submitted cansernipg t h e e f f o r t s proposed by each c o n t r a c t o r i n the a r e a s of n a v i g a t i o n , remote c o n t r o l o p e r a t i o n , and hazard avoidance. I n a d d i t i o n , r e q u e s t s f o r s u p p o r t i n g r e s e a r c h funds were made i n t h e a r e a s of (1) pre-programmed c o n t r o l s t r a t e g i e s f o r reducing t h e work load on t h e earth-based o p e r a t o r of unmanned LRV'S, ( 2 ) improvement of LRV n a v i g a t i o n a l accuracy through updating and c o r r e l a t i o n , ( 3 ) computer s i m u l a t i o n of s u r f a c e movement of unmanned LRV's f o r t h e development of ecanornical and r a p i d means of a s s e s s i n g t h e dynamic performance of unmanned LRV'S under d i f f e r e n t modes of o p e r a t i o n , and (4) u s e of non-imaging s e n s o r s t o avoid t e r r a i n hazards t o continued m o b i l i t y which were not d e t e c t e d by v i s u a l or o t h e r s e n s o r s a t t h e l a s t d e c l s i o n p o i n t i n s t o p - g o o p e r a t i o n of a n unmanned LRV. In-house s t u d i e s i n s u p p o r t of t h e program a r e p r o g r e s s i n g . 2. Lunar T a r g e t i n g S t u d i e s - Northrop (Schedule Order 60) During t h e r e p o r t i n g i n t e r v a l , t h e c o n t r a c t o r was d i r e c t e d t o suspend h i s p r i o r invee t i g a t i o n s ( s e e item 63 and t e m p o r a r i l y r e d i r e c t h i s e f f o r t s t o s u p p o r t l u n a r t a r g e t i n g i n v e s t i g a t i o n s being conducted i n t h e d i v i s i o n . I n s u p p o r t of t h e s e Fnves t i g a t i o n s , t h e c o n t r a c t o r w i l l modify t h e 6-D in-house computer program used f o r t a r g e t i n g v e r i f i c a t i o n t o a n approximate 3-D program and a s c e r t a i n whether o r n o t t h e r e s u l t i n g �accuracy is operational t h a t i t has t o r y and w i tation. s u f f i c i e n t t o use t h e 3-D program i n c e r t a i n phases of t h e verification. E f f o r t s have been hampered by t h e time (5 weeks) taken t o g e t a copy o f 4 t h e program from t h e Computation Laboral l be f u r t h e r hampered'by the complEte l a c k of program documen- In-house e f f o F t s to. convert7,a t a r g e t i n g v e r i f i c a t i o n computer program t o t h e 1108 have b e e n suspended because of t h e u s e r ' s r e c e n t i n t e r e s t i n a n o t h e r program u n d e ~development. 3. Parameter op;im?zat?on (Schedule Order 64) Studies f o r ARI - Lockheed 1 The hybrid computer program employed i n t h i s s t u d y i s operat i o n a l . During t h i s r e p o r t i n g p e r i o d , a n i n i t i a l s e r i e s of p r o d u c t i o n runs was made t o d e f i n e t h e form of performance index t h a t w i l l b e s t f i t the design objectives. 4. T r a j e c t o r y Optimization - Northrop (Schedule Order 59) F i n a l c o p i e s of t h e r e p o r t on Runge-Kutta formulas f o r second-order d i f f e r e n t i a l e q u a t i o n s have been d i s t r i b u t e d . On January 1 4 , t h e c o n t r a c t o r gave a n o r a l p r e s e n t a t i o n t o a l l i n t e r e s t e d persons i n t h e d i v i s i o n . The t a l k covered work done over t h e p a s t year and concluded w i t h a summary of c u r r e n t p r o j e c t s and aims, C u r r e n t l y , the c o n t r a c t o r i s c o n t i n u i n g t h e i n v e s t i g a t i o n i n t o o b t a i n i n g expansions of Lagrange m u l t i p l i e r s i n terms of a n impulsive s o l u t i o n . S e v e r a l n e c e s s a r y b a s i c e q u a t i o n s have been s u c c e s s f u l l y d e r i v e d t o date. 5. C-Minimax Control a . The p o s s i b i l i t y of c o n v e r t i n g a c o n t r o l problem of t h e C-minimax type i n t o a n e q u i v a l e n t Mayer problem and s o l v i n g t h e l a t t e r problem v i a t h e techniques of t h e c a l c u l u s of v a r i a t i o n s i s being s t u d i e d ; problems a r i s e due t o t h e d i s c o n t i n u i t i e s i n t h e d e r i v a t i v e s of t h e s t a t e v a r i a b l e s i n t h e proposed f o r m u l a t i o n . A review of t e x t s and papers i n the f i e l d i s i n progress. b. General DynamicslConvair (NAS8-21456) Objectives: (1) To extend t h e C-Minimax t h e o r y t o determine C-Minimax performance i n t h e presence of inconipletely s p e c i f i e d d i s t u r b a n c e s ; ( 2 ) t o determine i f a n a n a l y t i c s o l u t i o n e x i s t s f o r C-Minimax performance f o r l i n e a r dynamical systems w i t h bounded c o n t r o l ; and (3) t o i n v e s t i g a t e t h e computational problems discovered t o e x i s t w i t h t h e c u r r e n t computational a l g o r i t h m s . . �S u f f i c i e n t c o n d i t i o n s fo? c o n t r o l of l i n e a r systems i n t h e presence of d i s t u r b a n c e s of known form s o as t o a t t a i n t h e s p e c i f i e d t e r m i n a l c o n d i t i o n s have been developed d u r i n g t h e r e p o r t i n g period and a r e being, i n v e s t i g a t e d t o determine t h e i r u t i l i t y . S m e theorems r e g a r d ing t h e r e d u c i b i l i t y of high-order Systems to e f f e c t i v e low-order s y s teme f o r c e r t a i n r e s t r i c t e d C-minfmax performance i n d i c e s have a l s o been developed. 6. Launch Vehicle Control a. S t a t i s t i c a l Wind Model - Hayes (NAS8-21444) Objectives C o n s t r u c t i o n of a wind model f o r use i n s t a t i s t i c a l a n a l y s i s of launch v e h i c l e performance. Data r e d u c t i o n on MSFC computers has been s t i c c e o s f u l l y completed. The reduced d a t a have been d e l i v e r e d , and t h e c o n t r a c t o r is c o n f i d e n t of completing t h e g o a l s of t h e s t u d y . Because of t h e time l o s t i n d a t a r e d u c t i o n , they have r e q u e s t e d and r e c e i v e d a one-month no-cost e x t e n s i o n f o r t h e c o n t r a c t . The f i n a l r e p o r t i s now expected a t t h e end of February. b. S a t u r n V/Apollo Load R e l i e f (Schedule Order 60) - Northrap The c o n t r a c t o r ' s e f f o r t s 'have been t e m p o r a r i l y r e d i r e c t e d from t h i s a r e a ( s e e item 2 above). P r i o r t o t h e r e d i r e c t i o n , t h e cont r a c t o r had completed p r e l i m i n a r y s t a t i s t i c a l response s t u d i e s of t h e proposed load r e l i e f c o n t r o l law f o r t h e S a t u r n po pol lo on RAAERO-D'S high-speed analog f a c i l i t y . I n i t i a l e v a l u a t i o n of t h e r e s u l t s w a s favorable. B. As trodynamics Branch 1. Broken-Plane T r a j e c t o r i e s (Lockheed) Work continued on t h e development and checkout of new subr o u t i n e s f o r t h e General Broken-Plane Computer Program. Equations were w r i t t e n and p r o g r a m e d t o t e l a r e t h e i n c l i n a t i o n of t h e d e p a r t u r e and a r r i v a l p l a n e t o t h e t r a n s f e r a n g l e and t h e p o s i t i o n of t h e d e p a r t u r e and a r r i v a l planes w i t h r e s p e c t t o t h e l i n e of nodes. A u s e r ' s manual f o r t h e LMSC Broken-Plane I n t e r p l a n e t a r y T r a j e c t o r y Program by J. D. P a r r o t t , LMSC/HREC ~ 1 4 8 5 0 0 ,December 1968, was completed and d e l i v e r e d Do R-AERO-GA, �2. Mission Design C h a r t s a . Work was completed on t h e paper e n t i t l e d , "The A s t r o dynamicis t 's Role V i s -A-Vis t h e Sys terns Engineer. " The paper was p r e s e n t e d a t t h e AIAA 7 t h Aerospace Sciences Meeting i n New York. b. Work i s c o n t i n u i n g on t h e g e n e r a t i o n and r e p r e s e n t a - t i o n of a s trodynamical parameters used i n m i s s i o n a n a l y s i s s t u d i e s . The d a t a r e p r e s e n t i n g Earth-Mars t r a n s f e r s w i l l be p r e s e n t e d over a 15-year c y c l e of 7 s y n o d i c p e r i o d s . The method of p r e s e n t a t i o n of t h e d a t a w i l l f o l l o w t h e procedure o u t l i n e d i n t h e paper mentioned i n (a) above. 3. I n t e r p l a n e t a r y N-Body Programs a. Program Development (Lockheed) Work continued on t h e checkout of t h e N-Body I n t e r p l a n e t a r y T r a j e c t o r y Program. It w a s converted t o F o r t r a n I V language, and checkout of t h e 11 d i f f e r e n t o p t i o n s is underway. Also, a n i n v e s t i g a t i o n of methods of g r a p h i c a l l y p r e s e n t i n g i n t e r p l a n e t a r y d a t a i s underway. b. I s o l a t i o n Routine and T a r g e t i n g S t u d i e s (Northrop) The summary r e p o r t is i n f i n a l p r e p a r a t i o n and w i l l be d e l i v e r e d t o c o g n i z a n t MSFC p e r s o n n e l when completed. 4. O r b i t a l T r a n s f e r (Lockheed) Work continued on t h e i n v e s t i g a t i o n of methods of g r a p h i c a l l y p r e s e n t i n g i n t e r p l a n e t a r y t r a j e c t o r y d a t a , s u c h t h a t t h e m e r i t s of d i r e c t s i n g l e - p l a n e , broken-plane and p l a n e t a r y swingby t r a n s i t s can be r a p i d l y a s s e s s e d f o r a g i v e n m i s s i o n o p p o r t u n i t y . Computer r o u t i n e s were developed t o p l o t t h e h e l i o c e n t r i c r a d i u s , l o n g i t u d e and d i f f e r e n c e i n l o n g i t u d e s between two g i v e n p l a n e t s . These w i l l be used i n p r e d i c t i n g p l a n e t a r y encounter d a t e s t h a t r e s u l t i n f a v o r a b l e i n t e r p l a n e t a r y transfers . 5. O r b i t s i n Non-Central F i e l d s E f f o r t s a r e s t i l l b e i n g made t o c h a r a c t e r i z e c o n v e n i e n t l y t h o s e t r a n s f o r m a t i o n s of Euclidean 3-space which w i l l g i v e r i s e t o no c r o s s - p r o d u c t s i n transformed momenta. �6. Abort and A 1 t e r n a t e Migsions (Boeing) A f i n a l r e p o r t from Boeing f a r SSR-222 w a s r e c e i v e d t h e f i r s t of December. he‘ ma@ ab j p c r i u e of t b i s s t u d y was t o d e s i g n a g i n g l e e q g i n e - o u ~ gu jdance pethod $ h a t ~ o n f s r m st o a l l known r e s fr i c t i o n s g e n g i t i v e t q chqgges i q m$ssion, environment, o r v e h i c l e . and i s ~ i m p l i c i t yand rnfnirnum i m p g ~ tgn the f l i g h t program were considered major d e s i g n g o a l s . q e gyidance metbads m on side red were t o s a t i s f y t h e r e q u i r e ments of succesgf y l f l i g h t throuqh t h e maximym dynamic prgssHre r e g i o n , and c o n d i t i o n s g t 8-Ie burnout which a r e a c c e p t a b l e f o r S - I I s t a g e f l i g h t . The p r e s e n t e q g i p e s o q t c h i q f r e e z e metbgd dpes n o t meet tFe l g t t e y r e g u i r e ment f o r a l l c a s e s of engiqe o u t . D a t a f o r t h e AS-504 v e h i c l e were used f o r t h i s phase of t h e gtydy. * nq The f ~ l l o w i q gengfpe-out guidaqce methods weFe s x d t e d and eyaluated: (2) B r o p e l l a n t d e p l e t i o q f q y c e n t e r engipe c u t o f f . (3) T i l t arrest a t c e p t e r engine c u t o f f , ( 4 ) Mpdified p i t c h ~ ~ l y n w j . qcfo e f f i c i e n t s . (5) $Eeeying m$qglfg?mgpt ~ @ ? c r e $ t i afqo l l a w i ~ gengine o p t . (6) S e p a r a t e c h i - f r e e z e s c h e d u l e f o r upper and l ~ w e renggne failures, The r e s u l t s were t h a t the s e g a r a t e c h i - f r e e z e s c k e d u l e f q r upper and lo we^ e n g j n e f a i l u r e s b e s t met phe engine-out guidqnce r e q q i r e ments w i t h o u t e x t e n s i v e f l i g h t prograni changes. There would n o t , however, be enough time t o implement2t h e ~ eclzangps on t h e 504 f l i g h t , and a new c h i f r e e z e s c h e d u l e was o f f e r e d a s a n a l t e r n a t i y e t o t h e e x i s t i n g one f o r t h e AS-504 f l i g h t . A copy of t h e r e p o r t ~ a n t a l n i n gt h e s e r e s u l t s wqs g i v e n t o R-AEROIF. The a l t e r n a t e c b i - f r e e z e s c h e d u l e f o r AS-504 w a s implemented and c o q s i d e r a t i o n of t h e q s e of a c h i - f r e e z e s c h e d u l e based on knowledge a£ an upper o r lower engine f a i l y r e f ~ f ru t u r e f l i g h t s was recommended. 7. O c c q l t a t i o n S t u d i e s (Lockheed) The Blqne t g ~ yO r b i t Des i g a and Occut t a t i o n Computer Program i s being mod j f i e d t o q q l ~ g l a t et h e occultation c h a r a c t e r i s t i c s qf a prgbe qn a h y p e r b o l i c sp$ngky of t h e t a r g e t p l q n e t . C h a r a c t e r i s t i c s w i l l be c a l c u l a t e d from t h e time t h e probe e n t e r s t h e p l a n e t ' s s p h e r e a f i n f l u ence t o t h e time it l e a v e s . �Guidance Theory Branch C. 1. Support C o n t r a c t S t u d i e s a. Lunar T a r g e t i n g Analysis Using QUOTA The l u n a r t a r g e t i n g a n a l y s i s using QUOTA is s t i l l plagued w i t h s e n s i t i v i t y problems. E f f o r t s a r e c o n t i n u i n g toward improving t h e s e c a n t i s o l a t i o n scheme. A s i n g l e - p r e c i s i o n v e r s i o n of t h e l u n a r t a r g e t ing program was g e n e r a t e d on t h e 1108 computer. E f f o r t s a r e b e i n g made t o c o n v e r t t h i s program t o double p r e c i s ion. b. Quasi-Optimal Guidance Study Documentation of t h e QUOTA guidance scheme has been i n i t i a t e d . The document w i l l b a s i c a l l y summarize t h e complete QUOTA scheme w i t h t h e main emphasis on t h e minimum time problem, o r b i t a l t r a n s f e r and rendezvous. A p p l i c a t i o n of QUOTA t o AAP type rendezvous m i s s i o n s i s s t i l l under s t u d y . c. O r b i t Trim Systems E r r o r Analysis An a n a l y t i c technique i n d i c a t e s t h a t e f f e c t s of a n o r b i t t r i m maneuver upon t h e n a v i g a t i o n u n c e r t a i n t i e s w i l l be q u i t e s m a l l . Three Monte C a r l o s i m u l a t i o n t e s t c a s e s t o v e r i f y t h i s r e s u l t a r e being run. V e r i f i c a t i o n of t h i s r e s u l t i s i m p o r t a n t , s i n c e i t provides a b a s i s f o r decoupling n a v i g a t i o n u n c e r t a i n t y e f f e c t s and e x e c u t i o n u n c e r t a i n t y effects . d. Optimal Guidance Study Work is c o n t i n u i n g on the checkout of t h e g e n e r a l t h r e e dimensional optimal o r b i t a l t r a n s f e r computer program. Also, e f f o r t s t o o b t a i n good i n i t i a l g u e s s e s f o r t h i s computer program u t i l i z i n g impulsive conic s o l u t i o n s i s continuing. 2. Contracts a. - IBM A p p l i c a t i o n of Numerical Methods t o Extend C a p a b i l i t i e s f o r Optimal Rocket Guidance During t h i s r e p o r t i n g p e r i o d , t h e improvements t o t h e f i n i t e t h r u s t optimal o r b i t a l t r a n s g e r deck which were i n c o r p o r a t e d d u r i n g t h e l a s t r e p o r t i n g p e r i o d have been completely checked o u t . The program w i l l converge v e r y r a p i d l y f o r a v a r i e t y of i n i t i a l c o n d i t i o n s (about 3 seconds per c a s e ) . E v a l u a t i o n of the d e c k ' s c a p a b i l i t i e s f o r low t h r u s t o r b i t t r a n s f e r s i s now underway. - �b. Lockheed - Rerldedtous ~uidance The d i g i t a l programming of the r e g u l a r i z e d e q u a t i o n s i s s t i l l under-going checkout. The kdugh d r a f t of t h e f i n a l r e p o r t is being started. c. North American The computer pkogtam fop corhputing oprimai f i a i t e t h r u s t o r b i t a l t r a n ~ f k r sby q u a s i - l i n e a r i z d t i d n is e s s e n t i a l l y cotK@lete a l t h o u g h i t s t i l l hGs dif f i c t i l t y cbhverging same i s o i a r e t l c a s e s . A14d, a d d i k i d n s t o t h e program f o r i n p u t and s u t p b t i n a $ B r i e t y bf syse&ms of u n i t s were conipleted d u r i h b t h i h t e p b r t i n g p e r i o d . Eahvefsicin af t h e &beihg Q R ~ $t o the 1108 is p r d g r w s i n g d t a f a s t e t r a t e kh&h $ h t i c i p a t e d ; s e v e r a l e r r d f e i n €He pwgkarn (Boeing c o r r e c t e d theSe errbrs a f t e r we r e c e i v e d the program) k e r e discovered and t h e s e have been c o r r e c t e d . ~ o k ht h e t a r g e t i n g o p t i o n Bad midcourse c a r r e c t i o n o p t i o n have been checketl Out w i t h card i n p u t . These o p t i o n s w i t h i n p u t from t a p e have n o t Been rllecked o u t . It iS hopgd t h a t t h i s program w i l l be completely k o m k r t e d and ready f o r R-AERO-F w i t h t n a few weeks. An i n v k s t i g a t i o n was inad& t o determine wHat chdnges t o t h e QRTP would b e r e q t i i l c d iri ofdef tei t a r g c k high p e r i l u n e t r ~ j e c t o r i e s . ~t a p p e a r s t h a t the progrdm h&3 the c d p a b i l i t y t o Handle t h i s type of missiari w i t h o u t modifying it. It isi planded t o t a r g e t a t e s t cage t o verify this. The patched c o n i c s o l u t i o n a£ ~ a m b e r t ' s prdblem i n v o l v i n g t h e use of p a + t i a l d c r i v d t i v e t r a n s i t i o n m a t r i c e s is now s p e k a t i o n a l . This program makes t h e i p a t c h a t t h e eiract "sphere of inflixence," n o t a t t h e u s u a l approximate "spEiere crf i n ~ l u e h c e . " A t p r e s e n t , t h e program has o n l y one s e t of bobndary+cbndittons which i t can S a t i s f y . This s e t i s a s p e c i f i c a t i o n of to and Ro p l u s tf and t h e a s s o c i a t e d s e l e n o c e n t r i c p o s i t i o n v e c t o r . A d d i t i o n a l boundary c o n d i t i d n s f o t more g e n e r a l erid condit f o h s a r e b e i n g added. Making use of t h e f a c t t h a t , i n t h e absence of atmosphere t h e right-hand s i d e s (RHS) of t h e COV d i f f e r e n t i a l e q u a t i o n s a r e independent of f i r s t d e r i v a t i v e s , s p e c i a l i z e d r o u r t h - o r d e r Runge-Kutta formulas r e q u i r i n g o n l y t h r e e e v a l u a t i o n s of t h e RHS can be used. The R i t h a r d s o n e x t r a p o l a t i o n t h e n becomes a t t r a c t i v e a s a s t e p - s i z e c o n t r o l . TH&e f e a t u r e 8 haQe been used i n Peprogrdmming t h e three-dimensional COV deek t o o b t a i n a f a s t - r u h n i n g d&ck f o r t h e SDS-930 u s i n g a t r l r i a b l e s t e p 31te. Td i l l t i s t r a t e t h e efEectiveries8 ijf t h e repr6gratrmiing, 7000 second �coast-burn-coast-burn t r a n s f e r s between two e l l i p t i c o r b i t s can b e accomplished i n l e s s than 3 seconds of computer time f o r 6 - d i g i t accuracy. The burn phases which l a s t l e s s than 300 seconds a r e i n t e g r a t e d i n one s t e p , a n d t h e c o a s t phases a r e i n t e g r a t e d i n 1000-second time s t e p s . This new program makes more p r a c t i c a l t h e s o l u t i o n of l e n g t h y t r a j e c t o r y problems s u c h a s t r a n s f e r s between e l l i p t i c o r b i t s and t r a n s f e r s between t h e e a r t h and moon on machines l i k e t h e SDS-930, which a r e s m a l l and slow compared t o c u r r e n t t h i r d g e n e r a t i o n computers. VII. DYNAMICS AND FLIGHT MECHANICS DIVISION A. Saturn V 1. Guidance a. T a r g e t i n g f o r S-IVB P r o p e l l a n t D e f i c i e n c y (New) I f f o r some contingency, t h e S-IVB a r r i v e s a t r e i g n i t i o n i n t h e e a r t h parking o r b i t w i t h i n s u f f i c i e n t f u e l t o complete t h e nominal t r a n s l u n a r i n j e c t i o n , t h e nominal m i s s i o n o r an a l t e r n a t e l u n a r m i s s i o n can be accomplished by u s e of t h e s p a c e c r a f t p r o p u l s i o n system (SPS). The type of a l t e r n a t e l u n a r m i s s i o n depends upon t h e SPS AV requirement. The AV r e q u i r e d i s n o t o n l y a f u n c t i o n of t h e p r o p e l l a n t d e f i c i e n c y of t h e S-IVB s t a g e , b u t a l s o a f u n c t i o n of how e f f i c i e n t t h e a v a i l a b l e S-IVB p r o p e l l a n t s a r e used. This c o n d i t i o n i s t h e primary r e a s o n t h a t MSC wants " t a r g e t update." Two s t u d i e s have been made t o determine how t o make t h e most e f f i c i e n t u s e of t h e a v a i l a b l e p r o p e l l a n t s . The Boeing Company d i d a s t u d y (SSR-230, "Real Time T a r g e t Update") where t h e traj e c t o r y was completely optimized based on t h e a v a i l a b l e p r o p e l l a n t s . The in-house s t u d y (R-AERO-DGA-13-68, "Target v e c t o r s y n c h r o n i z a t i o n f o r t h e l u n a r l a n d i n g m i s s i o n due t o S-IVB p r o p e l l a n t d e f i c i e n c y " ) was made t o move t h e t a r g e t v e c t o r i n o r d e r t o o b t a i n from a d i f f e r e n t approach: a more optimum burn. The two s t u d i e s gave e s s e n t i a l l y t h e same r e s u l t s . Both s t u d i e s showed t h a t t h e amount o f SPS f u e l r e q u i r e d t o complete some type of l u n a r m i s s i o n can be s i g n i f i c a n t l y reduced (30 p e r c e n t ) . The t a r g e t v e c t o r s y n c h r o n i z a t i o n approach can be accomplished w i t h i n LVDC. The e q u a t i o n s a r e simple and a r e t r i g g e r e d by B , p r o p e l l a n t d e f i c i e n c y , which can b e c a l c u l a t e d f a i r l y a c c u r a t e l y onboard. A s t u d y i s now underway t o determine t h e i n f l u e n c e of m i s s predicting the D. ( ~ ~ A / ~ o e i n g ) . �b. S t a t u s of Recommended Guidance Changes (New) R-AERO-DGA-12-68, " s a t u r n V Continuous Guidance U n t i l 3-11: C u t o f f , " November 6 , 1968, recomended c o n t i n u i n g guidance u n t i l S - I 1 c u t o f f e f f e c t i v e w i t h AS-404. T ~ F Sd i d n o t g e t i n t o t h e f l i g h t R-ASTR d i d i n c l u d e t h i s recommendation i n a program f o r AS-504. memorandum t o Mr. Duerr, I - V - I U , s p e l l i n g o u t i n f o r m a t i o n f o r use i n e s t a b l i s h i n g t h e LVDC f l i g h t program f o r t h e AS-505 mission. The recumnlendation t o r e d e f i n e t h e p r e d i c t e d burn time i n t h e S - I 1 s t a g e f o r t h e guidance e q u a t i o n s w i l l n o t be implemented However, b e f o r e AS-504. R-ASTR has s t a t e d t h a t t h i s w i l l be i n AS-506. no docunientation has been r e c e i v e d . (DOA) 2. ~ynaimiss and Control a. S-XI S t a g e POGO (New) O s c i l l a t i o n s i d e n t i f i e d on t h e AS-503 f l i g h t j u s t b e f o r e S-11 c u t o f f have n o t been i d e n t i f i e d as POGO. The 18 Hz l o n g i t u d i n a l mode amplitude w a s a p p a r e n t l y h i g h e r than u s u a l due t~ abnormal engine operat i o n , The v e h i c l e responge was v e r y complex w i t h l a r g e subharmonic c o n t e n t i n d i c a t i n g s i g n i f i c a n t n b n l i n e a r i t i e b . A l l paratneter changes between AS-504 and AS-503 which could make t h i s v i b r a t i o n worse w i l l be i n v e s t i g a t e d . (DDS b. Pl&tform Backup Using S p a c e c r a f t A t t i t u d e Reference (New) Because of t h e h i g h c r i t i c a l i t y a s s o c i a t e d w i t h a f a i l u r e of t h e S a t u r n V ST-124M p l a t f o r m , a backup a t t i t u d e r e f e r e n c e f o r v e h i c l e c o n t r o l is b e i n g considered t o enhanice crew s a f e t y . Prel i m i n a r y s t u d i e s have i n d i c a t e d f e a s i b i l i t y , and follow-on s t u d i e s a r e b e i n g planned, A p r e l i m i n a r y scope f o r t h e s t u d i e s and p r e l i m i n a r y he a r e a s needing ground r u l e s f o r implementation have been d i s c u s s e d . more d e t a i l e d s t u d i e s and i n f o r m a t i o n concerning t h e s p a c e c r a f t systems needed from MSC t o perform t h e s e s t u d i e s have been i d e n t i f i e d , E a r l i e s t (~C/~~/Astrionics) e f f e c t i v i t y f o r t h i s backup i s now s e t f o r AS-506. 3. P r o j e c t I n f o r m a t i o n A p p l i c a b l e t o Many Vehicles S a t u r n y.. Rigid, Body Respons-e Anal ys is (New) : The r i g i d body response t o winds of t h e S a t u r n V launch v e h i c l e i n f l i g h t condiindividual t i o i s near c e n t e r engine c u t o f f i s betng examined c l o s e l y . per t u r b a t i o n c a s e s a r e being i n v e s t i g a t e d t o determine t h e RSS condit i o n s f o r t h i s maximum l o f l g i t u d i n a l a c c e l e r a t i o n case. The s t r u c t u r a l s a f e t y margin i n t h i s f l i g h t r e g i o n i s r a t h e r s e n s i t i v e t o a s l i g h t �b u i l d u p i n bending moment due t o c o n t r o l d e f l e c t i o n a n g l e s brought a b o u t by d i s t u r b a n c e o r misalignment. (DC) 4. P r o j e c t Information A p p l i c a b l e t o I n d i v i d u a l Vehicles a. AS-504 S t a b i l i t y Analyses (New) Recent i n v e s t i g a t i o n of t h e s t a b i l i t y of t h e AS-504 v e h i c l e has r e v e a l e d t h a t coupling between t h e bending and s l o s h i n g modes of t h e v e h i c l e has a s i g n i f i c a n t e f f e c t upon r e l a t i v e s t a b i l i t y . Some p r e v i o u s work on e a r l y c o n t r o l c o n f i g u r a t i o n s and v e h i c l e d a t a had l e d t o t h e c o n c l u s i o n t h a t , even w i t h t h e r e d u c t i o n i n s t a b i l i t y margins due t o i n c l u d i n g t h e coupling e f f e c t s i n t h e a n a l y s i s , v e r y adequate margins were s t i l l m a i n t a i n e d , and t h e r e f o r e t h e i n c r e a s e d complexity of t h e coupling s i m u l a t i o n could be dispensed w i t h t o reduce t h e volume of d a t a t o be handled. A f t e r many i t e r a t i o n s , however, t h e adequate margins have d i s a p p e a r e d , and t h e now s i g n i f i c a n t e f f e c t s of coupling must be included i n t h e s i m u l a t i o n s . With t h e i n c l u s i o n of s l o s h / b e n d i n g c o u p l i n g , the s l o s h modes of t h e AS-504 couple t o produce a s l i g h t l y u n s t a b l e s l o s h mode f o r t h e damping p r e d i c t e d f o r a n 0.05-meter s l o s h wave h e i g h t u s i n g nominal v e h i c l e parameter v a l u e s (AS-503 shows t h e same ind i c a t i a n s w i t h s i m i l a r a n a l y s e s ) . Allowance f o r parameter v a r i a n c e s produces a n u n d e s i r a b l y l a r g e i n s t a b i l i t y f o r t h e f ixed-time, 1i n e a r a n a l y s i s used. However, s l o s h damping i n c r e a s e s as wave h e i g h t i n c r e a s e s , and a l i m i t c y c l e w i l l be reached i n t h e s t e a d y s t a t e i f t h e degree of i n s t a b i l i t y i s n o t t o o g r e a t . Response s t u d i e s f o r one - ( r a t h e r a r b i t r a r y ) method of r e p r e s e n t i n g t h e 30 parameter v a r i a t i o n s , u s i n g measured Jimsphere winds t o f o r c e t h e s y s tem, have shown t h a t t h e i n c r e a s e i n damping due t o t h e i n c r e a s e d wave h e i g h t is s u f f i c i e n t t o (~~/Astrionics/ p r e v e n t dangerous b u i l d u p s of s l o s h i n g p r o p e l l a n t s . Boe ing) b. AS-504 Third S t a g e Bending A n a l y s i s (Ref. F e b r u a r y l ~ a r c h1968, p. 38) A v i b r a t i o n a n a l y s i s has been made of t h e t h i r d f l i g h t s t a g e S a t u r n V/AS-504 ( w i t h LES a t t a c h e d ) . This c o n f i g u r a t i o n would occur i f c e r t a i n m a l f u n c t i o n s e x i s t e d i n e a r l i e r s t a g e s . Consequently, t h e dynamic c h a r a c t e r i s t i c s a r e n e c e s s a r y f o r c o n t r o l system v e r i f i c a t i o n . The r e s u l t s of t h i s a n a l y s i s a r e being p u b l i s h e d . (DDS) c. Dynamic Data f o r AS-504 M i s s i o n D, S-IVB S t a g e h A f t e r Payload S e p a r a t i o n (Ref. ~ e b r u a r y l ~ a r c1968, P* 38) Bending and t o r s i o n d a t a f o r AS-504 Mission D, S-IVB s t a g e a f t e r payload s e p a r a t i o n , have been p u b l i s h e d i n memorandum ~ - A E ~ 0 - ~ ~ - 1 4 8 - 6 Included 8. w i t h t h e d a t a a r e t h e t o l e r a n c e s and damping t o be used f o r c o n t r o l system v e r i f i c a t i o n . (DDS) �B. S a t u r n Apollo A p p l i c a t i o n s Program 1, Cluster a. Missiorl P r o f i l e (1) AAP Experiments Data Bank (Ref. ~ c t o b e r / ~ o v e m b e r 1968, p. 42) The AAP experiments d a t a bank has been r e v i s e d t o i n c o r p o r a t e v a r i o b s s u g g e s t i o n s and camtrierits t o make i t more meaningful. The r e v i s i o t l is now b e i n g e v a l u a t e d by R-AERO-DAM. This e v a l u a t i o n w i l l be forwarded t o ~ a r t i n / M a r i e t t aC o r p o r a t i o n f o r implementatibn s o t h a t t h e f i n a l v e r s i o n w i l l be a c c u r a t e and up t o d a t e . This v e r s i o n w i l l have wide d i s t r i b u t i o n and w i l l represent t h e l a s t i t e r a t i o n and docu(DAM/Martin) m e n t a t i o n of t h e d a t a bank. (2) nes i&n Reference Miss i o n Document (DRMD) AAP-l/AAP-2 (Ref. April/May 1968, p. 42) Change 1 t o r e v i s i o n B of t h e DIWD was made t o add t h e a n a l y s i s of t h e A i r l o c k Module ~ i e c t r i c a lPower System Consuma b l e s and t o r e v i d e f u e l c e l l cryogenic requirements. Copies w i l l be s e h t t o a l l who r e c e i v e d t h e o r i e i n a l i s s u e . (~A~fMartFn) (3) Exper imant C o n i p a t i b i l i t y (Ref. October/November 1968, p , 43) . The r e s u l t $ of t h e experiment/mission c o m p a t i b i l i t y a a a l y s i s were p r e s e n t e d t o t h e Manned Spaee F l i g h t Experiment Board (MSFEB). The MSFEB, a c t i n g upan r e e a m e n $ % t f o n s made i n the s t u d y , chose one of t h e o p t i o n s t o be included i n t h e new Mission D i r e c t i v e 3D; t h e o p t i o n chosen d e f i n e d a new b a s e l i n e of experiments f o r t h e m i s s i o n AAP-1/AAP- 2 and AAP-3A. (hAM) (4) Missfon AAP-3/AAP-4 Timeline Analysis (New) The l a g i c f o r a new a u t o m a t i c experiment s c h e d u l e r w a s developed f o r the ATM-type m f s s i o n . This prbgram w i l l i r i t e r r o g a t e an e v e n t i n p u t , such a s s o l a r f l a r e s , and w i l l s c h e d u l e t h e experiment. A l ~ h o u g ht h e program has been developed p r i m a r i l y f o r t h e ATM package, i t can a l s o be used i n connection w i t h any event--oriented program ( i . e . , e a r t h resources). The program 2s being developed by M a r t i n / ~ a r i e t t a C o r p o r a t i o n (MMC), Denver, i n s u p p o r t of t h e i n t e g r a t i o n c o n t r a c t . (Drn/rnC ) �(5) The Markov Chain S a t u r n V Apollo Mission Success P r o b a b i l i t y Model (New) The s k e l e t o n computer program c o n t a i n i n g t h e b a s i c i n g r e d i e n t s of t h e f i n a l program has been completely checked o u t . The countdown model has been coded, and t h e r e s u l t i n g computer program is b e i n g checked o u t . The i n p u t scheme i n t r o d u c e s f a i l u r e r a t e d a t a f o r each subsys tem v i a c a r d s o r tape. These f a i l u r e r a t e d a t a and a n a r b i t r a r y time i n t e r v a l a r e then used t o compute t h e countdown t r a n s i t i o n p r o b a b i l i t i e s , which a r e t h e n s t o r e d on t a p e f o r l a t e r use. Tape updating s u b r o u t i n e s a r e being p r o g r a m e d . The s t u d y i s expected t o be complete i n about a month ( c o n t r a c t t e r m i n a t e s March 10, 1969). (DAM/ ~ o c k h e e d) (6) AAP Hardware U t i l i z a t i o n (Ref. OctoberlNovember 1968, p. 4 3 ) The o v e r a l l flow showing hardware u t i l i z a t i o n i n t h e Apollo A p p l i c a t i o n s Program f o r contingency and backup m i s s i o n planning has been completed. The o b j e c t i v e of t h i s m i c r o l o g i c i s t o determine t h e p r o b a b i l i t y of s u c c e s s of 2 b a s e l i n e AAP m i s s i o n a s a f u n c t i o n of t h e hardware a v a i l a b l e . The more d e t a i l e d m i c r o l o g i c which i n t e g r a t e s t h e hardware s u c c e s s and f a i l u r e s i n t o t h e program is n e a r completion. Pro(DAM) g r a m i n g of t h e problem f o r t h e IBM 1108 has begun. (7) Lockheed FORRCAST Computer Program (New) The f i r s t t h r e e f i l e s of t h e FORRCAST Computer Program a r e now o p e r a t i n g on t h e IBM 1108. These f i l e s c o n s i s t of (1) t h e ephemeris g e n e r a t o r , (2) t h e t i m e l i n e of t a r g e t l s t a t i o n t a b l e s g e n e r a t o r , and (3) t h e a s t r o n a u t s c h e d u l e r program. A f a m i l y of check a s t r o n a u t t i m e l i n e c a s e s a r e b e i n g r u n u s i n g b a s e l i n e experiment d a t a from t h e AAP 1 / 2 mission. A simple check c a s e has been r u n s u c c e s s f u l l y , and t h e (DAM/ s c h e d u l e s should now be a b l e t o handle p r e s e n t t i m e l i n e problems. Lockheed) (8) AAP-2 Launch Vehicle Performance A n a l y s i s (New) The launch v e h i c l e performance a n a l y s i s f o r AAP-2 ( O r b i t a l Workshop) has been completed and d i s t r i b u t e d i n R-AERO-DAP-1-69. Maximum l o n g i t u d i n a l a c c e l e r a t i o n , dynamic p r e s s u r e (with and w i t h o u t w i n d s ) , and aerodynamic h e a t i n g i n d i c a t o r d e s i g n t r a j e c t o r i e s a l o n g w i t h t h e f l i g h t performance r e s e r v e s were determined. F l i g h t performance r e s e r v e s a r e computed f o r b o t h open- and closed-loop PU o p e r a t i o n . The launch v e h i c l e i n s e r t s i n t o a 185 x 193 n a u t i c a l m i l e a l t i t u d e o r b i t w i t h S t u d i e s a r e being i n i t i a t e d f o r t h e manned AAP a n i n c l i n a t i o n of 35'. launches t o d e f i n e d e s i g n c r i t e r i a and FPR requirements. (~AP/~hrysler) �(9) AAP-1, 2 , 3A, 3 apd 4 F l i g h t P r o f i l e and Launch Window Analysis (Ref. October/November 1968, P . 41) The AAP c i u s t e r q & s i o n p r e l i n l i q a r y f l i g h t p r o f i l e and launch window a n a l ys is i s c o n t i n u i n g The OWS o r b i t a l i n c l i q a t i o n has p r e v i p u s l y been d e f i n e d t o s a t i s f y t h e AAP-1 and 2 optimum launch requirements. The AAP-3A @-phase lqunch o p p o r t u n i t y f o r t h e nominal rendezvous p r o f t l e o c c u r r i q g a p p r o x b a t e l y 9Q days a f t e r t h e U P - 1 launch and r e q u i r i n g t h e s m a l l e s t amouqt QE nodg change occurs a t 22:51 GMT on day 94. This launch o p p o r t ~ n i t yoccurs approximately 9 minutes b e f o r e t h e optipum launch t i p e and causes q paylbad l o s s of approximately l O O Q pounds f o r AAP-?A. The e f f e c t s f adding a c i r c u l a r i z a t i o n paneyver a t gpogee of t h e i n s e r p i p n qrblf ($1 x $20 NM) of t h e nominal repdezvqus p r o f i l e and c o a s t l p ~i n t h i p qrbgt i s being i n v e s t i g a t e d . By c o a s t i n g i n t h i s o r k i p , the pn-phaqa l a q p ~ h~ p p o r f u n i t yw i l l pccur n e a r e r t h e optimum launch o p p p ~ P v n i t y , tbua g a i q i o g U P - 3 A payloqd, b u t r e q u i r i n g (F)A0/~A~/Nprfhr~p) more rendezvous twe. . (1Qf Mechanizat$an of t h e C l u s t e r pliasion P r o f i l e and "bapnch Window Anqlysis (Ref. Ocrober/ Vavember 1968, p. 41-42] The l o g i e Flpw prgv$gusly developed £or t h e d r i v e r o r e x e c u t i v e proFram n e c e s s a r y goy Eh$q mechanj.aation bas been p r o g r a m e d . The purpose of t h e d r i v e r i s $a tfgnqfga: data between t h e O r b i t a l Bredict i o n , QgSck Look, and ROBOT @FQ$FWS. T h i ~daga t r a g a f e r is now being performed by hand. The development of t h e d r i v e r has made i g n e c e s s a r y t o develqp c o w o n b l o c k s f o r each program and Che d r i v e r i n o r d e r t o make t h e d a r a t r a n s f e r bqtween prQgFams p o s s i b l e . Also, n a m e - l i s t i n p u t c a p a b i l i t y has been added t o t h e p r b g r w s t o f a c i l i p a t e t h e d a t a t r a n s f e r Cgpputey rpns a r e being made t o check phis o u t . between prOgraRS. (DAQLNO~ throp) (11) LM Repdozvous A t t i t u d e P r o f i l e (New) Work is underway t o determine t h e a t t i t u d e of t h e This i n p u t is t o be used as Jnput ts a thermal a n a l y s i s of t h e LM d u r i n g rendezvous. I n t h i s a n g l y s j s , two d i f f e r e n t methods of readezvous a r e being considered (Hybrid S t a b l e O r b i t and M = 3), and t h e maximum d e v i a t i o n s from t h e nominal w i l l b e analyzed i n each case t o provide l i m i t s on t h e sun (DAO) angle, Di w i t h r e p p e c t t o t h e s u n d u r i n g rendeavpus. �(12) SO27 (New) An a n a l y s i s has been made t o f i n d t h e s e p a r a t i o n between t h e LM and S-IVB as a f u n c t i o n of time a f t e r p r o p u l s i v e dumping from t h e s p e n t S-IVB. The impulse from t h e dump w a s g i v e n i n b o t h t h e p o s i g r a d e and r e t r o g r a d e d i r e c t i o n s , and t h e growth of t h e s e p a r a t i o n a s a f u n c t i o n of time i s symmetrical i n t h e two c a s e s e x c e p t i n one case t h e S-IVB l a g s t h e LM (posigrade impulse) and i n the o t h e r c a s e t h e S-IVB l e a d s t h e LM. For nominal performance of t h e launch v e h i c l e t o o r b i t , enough p r o p e l l a n t is l e f t i n t h e S-IVB t o g i v e a n impulse of 19.4 m / s . For a -30 performance of t h e launch v e h i c l e , a n impulse of 12 m/s is o b t a i n e d and f o r a +3a performance of t h e launch v e h i c l e , an impulse of 26 m / s i s o b t a i n e d . The growth i n s e p a r a t i o n as a f u n c t i o n of time r a n g e s from approximately 113 minute p e r o r b i t f o r -30 performance t o approximately 1 minute p e r o r b i t f o r +30 performance. The times j u s t mentioned a r e t h e approximate d i f f e r e n c e s i n time when t h e two o b j e c t s pass a g i v e n p o i n t (say, a t r a c k i n g s t a t i o n ) . (DAO) (13) S o l a r Observation Times and Out-of-Plane Angles (New) To supplement t h e AAP f l i g h t p r o f i l e and launch window a n a l y s e s , d a t a have been g e n e r a t e d f o r a n o r b i t a l i n c l i n a t i o n of 35O, y i e l d i n g s e t s of curves such t h a t : Given any launch d a t e and launch time, d u r i n g t h e y e a r 1972, one may determine t h e p e r c e n t a g e of time a v e h i c l e spends i n t h e s u n l i g h t f o r any day d u r i n g t h e m i s s i o n and t h e out-of-plane a n g l e , @ (which is d e f i n e d a s t h e a n g l e between t h e o r b i t a l plane and t h e s o l a r v e c t o r ) , f o r any day d u r i n g t h e mission. Given any launch d a t e i n 1972, one may determine t h e t o t a l time s p e n t i n t h e s u n l i g h t f o r a 56-day m i s s i o n (minimum and maximum) corresponding t o two launch times d u r i n g t h e day. A memorandum d i s p l a y i n g t h e s e curves is now being prepared. The program used f o r g e n e r a t i n g t h e s e curves c o n t a i n s a subr o u t i n e which can c a l c u l a t e t h e r i g h t a s c e n s i o n and d e c l i n a t i o n of t h e sun f o r a g i v e n J u l i a n d a t e . (DAO) b. Guidance (1) S-IVB/CSM Guidance C o m p a t i b i l i t y Study (New) The e q u a t i o n s and computer programs d e s c r i b i n g Hohmann/cross-product s t e e r i n g guidance used i n our s t u d y of t h e S-IVB/ CSM guidance c o m p a t i b i l i t y s t u d y f o r AAP-3 have been documented. The memorandum has been g i v e n t o t h e C h r y s l e r Corporation Space D i v i s i o n f o r (DGA) u s e i n AAP s t u d i e s u n t i l more i n f o r m a t i o n is r e c e i v e d from MSC. �(2) A d d i t i o n t o and V a r i a t i o n of t h e Lambert Problbm (New) Th& ~titnlj6rtptoblem d e a l s w i t h d e f i n i n g a Conic betweefi h a p d g i f i o n v e c t d f d wh&n: kh& time i s s p e c i f i e d . Th& &s$hmptions a r e t h e ihvCrS'e squake law1 3rd thd<t i h e a f a r r i v a l is t h e " f i r s t time" of a r r i v a l . w i t h t h i s a s e d i p t i o n , t h e cbnid i s unique. HoweverI i f t h e d t h i t i h e bf i r f i v a l oh t h e dgeond (or time of a r r i v g l i g ~ @ & e i f i gas more) pass ( m h l b i d f b l t ) , LHen tH@ cBiiFc id hrit lihique an*al.$. I n thbst c a s e s , t h e r e afk kw6 6 o l i t t F ~ n s . A komputer progrim, which It$$ beeh developed t o deEtirni%ric ill1 d b l c l t i b n ~iS ~ eixpeeted t o b e used i n sonie AAP s t u d i e s ; The kh&bert pPobl&ih nkgledkb thk o b l d t e n e s s e f f b c t of t h e edetH and bklie? ~ e k t b f b i h g&!Ef$cfs. W h ~ p u k e rpro@lil& has beeti d e i e l o p e d t o p r c d F t t t h e dbi&t6fi$!4b @ff&ck# by h i n & ~i.ick8'itikthbd of r & c t i f i c i r t i c j l i . 'I%$@ tkehtlique i b b e i h g ii!3kd With thk ~ a n i b & %~boblem t i n Idiite &I? g t c i d i ~ ~ :~ h $ d$pt-~j;&khcgh bi! dsed i n kibsk f k @ t i - f l i g k t . t r a j e c t d r y ehl&til&fi 6 i i g ; (B@A!#bkthro#) 1 ~38 kuidaake d a v i g h t i b n Hdrdw&i-e f3) ~ p - 3, ~ d n p itt i5 it i ty Akalgs is (New) The s o f t w a f e (kqddtiorid) c m p c i t i b k l ~ t j fbf t h e CSM c r o s s - p r o d u c t s te@?irig w i t H f@l B teekitig hi39 d l r e a d y be&i ei3 t g b l i s h e d , b u t t h e p l a t f o r m a i i g f h e n t etFdEB of thk e$h '&fU p l & r e s a reijuireniknt on t h e d21m s t a g @ kb eiigbrc$ tH(3 &!liked ~ ~ ~ ~pldne i k dl tl d - f a dtbge dubd r b i k a l ctitdff. THk fMU tHd.3 k6HPiikE8 &he i h s t a i i k 6 W b ~ #plhne and st@k?B i n t h i d p l a n e t o a c h i e v e o r b i t P 1 i n i e r t i ~ i i , To e s t a b l i s h t h e accuracy of the riatripational S t a t e a t s ' I ~ ~ B c u t o f f , h diiai n a v i g a t i o i i system s i m t i i a t i d n is r e q u i r e d w i t h t W i h U i h i3 mmdnit6r mode d u r i n g 3-IB dnd t d t h e l'bll.7 a t c ~ H ignition s - ~ ~ T I S s t a g e b o o s t efivlronmeht: R &v?lEcB~V&r and subsequent cohput&tion bf t h e reniaining t r a j e c t o r y t o o t b f t a l ih3ertibfi Q r e r 6 q h i r e d i n dkdei- t o e v a l h d t e t h e a c c u r a t y 6f t h e i n s e r tibn orbit. (~GG/Na?throp) c. Dyhamids dhd Codtrol (1) Mcknefikurn M&nagSiiIektt ( R k f . ~ c t o b e r / ~ o v e t h b e1968, r p. 44245) ~ t u d i ' l 3 sa r e continuing on t h e l i n e a r giffibal arid rrds3-feedback laws, which a r e dekigned t o e l i m i n a t e t h e problems of a n t i - 2 j a r a l l e l i s m and h i t t i n g ginibal stop^. LOSS o f c o n t r o l may i - e s u l t i n e i t h e r ease. The advankage O£ tii&Se laws over t h e ones c u r r e n t l y i n use id t h e i r s i i h ' p l i e i t y w i t h no h&@tni"ri$ d6gkddation i n o v e r a l l sydtem reswhse. �Comparison r e s u l t s obtained thus f a r have been w i t h o u t bending f i l t e r s i n t h e forward loop. Bending f i l t e r s a r e b e i n g included and cross-checks w i t h A s t r i o n i c s Laboratory w i l l be made. (DDD/Northrop) (2) S t r u c t u r a l Damping P r e d i c t i o n s (Ref. October/ November 1968, p. 48) The m a t e r i a l damping program has been checked o u t . The i n p u t d a t a f o r computing t h e m a t e r i a l damping of the s o l a r p a n e l s f o r the ATM were g e n e r a t e d u s i n g t h e frame s t r u c t u r a l a n a l y s i s program. Design of t h e j o i n t t e s t f i x t u r e s was completed. (DDS/~ockheed) F a b r i c a t i o n of t e s t f i x t u r e s is a b o u t 40 p e r c e n t complete. (3) Impulse Requirements (New) The impulse r e q u i r e d t o hold t h e c l u s t e r w i t h t h e ATM docked t o P o r t I is being determined. The c u r r e n t t h i n k i n g i s t o s p i n up t h e CMG's w i t h t h e c l u s t e r i n a s o l a r i n e r t i a l hold as opposed t o X-POP. Since t h e a n g l e between t h e sun l i n e and t h e o r b i t a l p l a n e i s not known, t h e impulse r e q u i r e d f o r CMG spin-up must be o b t a i n e d f o r a range of @ a n g l e s from 0 t o 60 d e g r e e s . (DDD) d. P r o j e c t Information Applicable t o I n d i v i d u a l Vehicles (1) U P - 2 Response Analyses (October/November 1968, P* 46) The AAP-2 launch v e h i c l e f i r s t f l i g h t s t a g e is b e i n g i n v e s t i g a t e d i n terms of v e h i c l e responses t o measured wind p r o f i l e s on t h e h i g h speed analog computer. Gain changes i n c o n j u n c t i o n w i t h a l r e a d y e s t a b 1 i s h e d c o n t r o l networks w i l l be i n v e s t i g a t e d i n a n a t t e m p t t o p r e v e n t c o n t r o l l a b i l i t y problems i n t h e maximum dynamic p r e s s u r e r e g i o n of f l i g h t . Rigid body responses t o a 50 p e r c e n t i l e wind p r o f i l e a r e being checked a g a i n s t those obtained from a d i g i t a l s i m u l a t i o n . The c o m p i l a t i o n of f l e x i b l e body d a t a f o r u s e i n t h e a n a l y s i s i s a l s o i n progress. (DC) (2) AAP-2 Shroud J e t t i s o n (Augus t/September , p . 43) S i n c e t h e l a s t s t u d y of t h e AAP-2 shroud j e t t i s o n (published i n R-AERO-10-68, October 9, 1968), more r e c e n t i n f o r m a t i o n has r e v e a l e d t h a t t h e r e w i l l be an u m b i l i c a l d i s c o n n e c t f o r c e of approxim a t e l y 500 pounds a c t i n g a t t h e mouldline near v e h i c l e p o s i t i o n 11. This has n o t been considered i n any of t h e previous s t u d i e s . The e f f e c t of t h i s d i s c o n n e c t f o r c e on t h e s h r o u d - j e t t i s o n o p e r a t i o n i s b e i n g s t u d i e d . A preload d e v i c e t o a l l e v i a t e t h i s . f o r c e w i l l be considered i f t h e pre(DC) s e n t s t u d y i n d i c a t e d i t s need. �(3) AAP-4 LPIIATM S e p a r a t i o n From Launch Vehicle (New) E j e c p i a n Q£ t h e LM/A@ from t h e 3-IVB s t a g e w i t h t h e A p s l l o s p r i n g s y s tam i e beiqg s t u d i e d f o r adequacy. This a e p a c a t i ~ n s i m u l a t i o n i n v o l v p s ti imu@pion pf e i e c t r i c a l and pneumatic y m b i l t c a l d i s connectq which r e s i s t s e p g f q t i a n w i t h a t o t a l f o r c e a s l a r g e a6 r h a t of one of t h e f o u r maip s e p a r a t i o n ' ap$ings. 4 preload d e v i c e t o c o u n t e r a c t t h e u m b i l i c a l d$sconnect fgjrce i p being designed. Tbis s t u d y is t o e s t a b l i s h d e s i g n c r i t e r i a f o r t h e p y e l ~ a dd e v i ~ eand t o v e r i $ y t h e f e a s i b i l i t y o f A q e j e c t i o nw i t h t h e ~ h b l l as p r i n g system. (DC) 2. OWS 3-XKB Workshop 4lnsFFnp ppring Powered P l i g h t (&pf. Auguntbf3eptember '19682 p. 45) a. The a x p e r i w n f $ l $nve%t$g&fionof $he podel8 of t h e f o o d , waste management, aqd wsrk areas i s ppw complete. Tho d a t a f o r t h e work a r e a cornpagefneet heve been reduged, apd peqhapicgtl model has ~ b i si q t h e lgpges t and' b a s t i g t r i c a ~ e l yqhaped t a n k been i d e n t i f i e d compartment. Three @lash frequppcies f q i z l y c l o s e t o g e t h e r have been i d e n t i f i e d , and these poded g r e a e n s i t i y e FD t h e d l r e c t i o g q f e x c i t a t i o ~ . The mechanical model f o r t h i s p g g t i o n of the tank is comgqoed of t h r e e spring-mass-damper eyg terns an4 pwo r$g+d Isasses. The over311 s l o s h model f a r t h e e n t i r e p a r t i t i a n @ @g e p F h p @ likely t o be q q i t e ' complgx. ( ~ ~ 8 / 6 0 u t h w-te sResearch In@ t l g y g p ) . b. Wo~kfhopC o n t r o l S i m u l a t i o p (New) A ~ c u d yhqs hepp ~ ~ n d q s ~ pu sgi nl g~ a d i g i t a l Gomputer program, t o s i m u l a t e t h e S-IVB c o f l t r o l s y s k s ~ ,t h e aeradynag$.c t b r q u e s a c t i n g an t h e v e h i c l e , and thg d e n s i t y p r b f i l e , The r e s u l t s pf phis s t u d y , npmely, t h e hapulse r e q u i r e d f a r c o n t r o l and i-qaneuvgre, have been compared w i t h t h e 5(92/S-IV'@ f l i g h t d a t a , A memorandum g i v i n g t h e s e r e s u l t s w i l l be p u b l i s h e d gpoa. (DDD) c. vass Parameter S e n s i t i v L t y- (Ref. , Qctober/Noyember 1968, P. 4 6 ) The WACS impulse was found t o be v e r y s e n s i t i v e t o m o p n t s of i n e r t i a , I2 and 13. v a r i a t i o n s i n t h e two l a r g e s t The d i s t u r b a n c e t o r q u e is' a Sunctign af s e v e r a l q u a n t i t i e s , one ef which is ,the d i f f e r e n c e between these promenf;s of i n e r t i a (I2 Ig), A 15 p e r c e n t i n o r e a s e i n (I2 T3$ c a u s e s a la $crease i n t h e r e q u t r e d impulse p e r orbst. The increase qf 15 p e r e g n t can be r e a l i z e d i f t h e l 8 r g e r of the z@owqts is iincyeered by 112 percenp, These comments have been r e g a r t e d 6n plernorc~nx9umR-&E~~o-DQ-1434.3 , "Cs f - t i c a l I n e r tfa Proper t i e s - - �During AAP C l u s t e r Mission," November 27, 1968. A more d e t a i l e d a n a l y s i s i s i n p r o g r e s s and t h e r e s u l t s w i l l be r e p o r t e d l a t e r . (DDD) d. A c t i v e Control (Reference ~ c t o b e r / ~ o v e m b e1968, r p. 45) Checkout of a program t o e v a l u a t e OWS/ATMmomentum dumping schemes u s i n g g r a v i t y g r a d i e n t torques i s n e a r i n g completion. Momentum management over more than 12 o r b i t s has been simulated s u c c e s s f u l l y . The a n g u l a r momentum of the CMG's which accumulates d u r i n g t h e l i g h t p o r t i o n of a n o r b i t i s reduced s u b s t a n t i a l l y d u r i n g t h e d a r k p o r t i o n of an o r b i t . Minor i n c o n s i s t e n c i e s i n t h e r e s u l t s a r e b e i n g c o r r e c t e d . A d e t a i l e d r e p o r t p r e s e n t i n g t h e t h e o r y of t h e b a s i c g r a v i t y g r a d i e n t momentum dumping method i s being published. The program t o e v a l u a t e v a r i o u s CMG momentum d i s t r i b u t i o n laws has been extended t o i n c l u d e t h e computation of power consumption and subsequent p l o t t i n g . A r e p o r t is being w r i t t e n on t h i s program. (DCA) a. Bending F i l t e r s (Ref. oct$~r/~ovemb& 1968, p. 44) A s e t of second o r d e r f i l t e r s has. been designed f o r t h e ATM based on a l i n e a r uncoupled s i m u l a t i o n . These f i l t e r s p r o v i d e f o r a 50 p e r c e n t v a r i a t i o n i n bending mode natuPa1 frequency and a 20 p e r c e n t v a r i a t i o n i n bending mode s l o p e , The r e s u l t s of t h i s s t u d y w i l l be published i n a memorandum. F u t u r e s t u d i e s w i l l i n c l u d e t h e e f f e c t s of (DDD) c r o s s - a x i s coupling and a l s o CMG backlash. b. P a s s i v e A t t i t u d e Control (Ref. October/November 1968, P a 45) A f e a s i b i l i t y s t u d y concerning t h e aerodynamic damping of an O r b i t a l Workshop type of s p a c e v e h i c l e u s i n g t h e s o l a r panels i s almost complete. A t o r s i o n a l s p r i n g and a v i s c o u s damper i n each of t h e s o l a r panel hinges r e s u l t i n e x c e l l e n t damping of t h e tumbling motion of t h e s p a c e c r a f t , a s i n d i c a t e d by a n a n a l y t i c a l o p t i m i z a t i o n s t u d y and by r e c e n t computer s i m u l a t i o n s . R o t a t i o n a l motion a b o u t a l l three-body axes i s s i m u l t a n e o u s l y damped by t h i s a t t r a c t i v e concept, which r e q u i r e s o n l y minor d e s i g n e f f o r t s and i s subs t a n t i a l l y l i g h t e r than o t h e r known concepts. A r e p o r t on t h e o p t i m i z a t i o n of c r i t i c a l d e s i g n parameters and s i m u l a t i o n r e s u l t s has been published. Minor m o d i f i c a t i o n s were made i n a computer program which i s e s p e c i a l l y e f f i c i e n t f o r s i m u l a t i n g t h e P a s s i v e Motion of O r b i t i n g S a t e l l i t e s (PAMOS) over long time p e r i o d s of 10 o r more o r b i t s . The m o d i f i c a t i o n s were aimed a t f u r t h e r reducing t h e computing time and a t maximum convenience i n t h e d a t a i n p u t s . �A b a s i c program f ~ t rh e s i m u l a t i o n of hinged s a t e l l i t e s is n e a r i n g completion. S i m p l i f i e d c a s e s have been r u n s u c c e s s f u l l y u s i n g b o t h Runge-Kutqa and Adams i n t e g r a t i o n packages. The i n p u t and o u t p u t r o u t i n e s have been modified and s e v e r a l o p t i o n s added t o (QCA) f a c i l i t a t e program use. c. AAP Uf/ATM Unmanned Rendezvous (Ref. ~ u n e / J u l y1968, p. 47, August/September 1968, p . 44, and October/ November 1968, p , 4 3 ) The f e a s t b i l i t y a n a l y s i s i s e s s e n t i a l l y completed s i n c e c a p a b i l i t y has been e s t a b 1 $shed Co perform 811 maneuvers r e q u i r e d of t h e S-IVB/LM-ATM t o rendeevqug w i t h t h e s r b i t a l gssembly. F u r t h e r s t u d y of t h e f o r m u l a t i o n of S g n i t i o n eguagCspq f q r q11 maneuver? i s r e q u i r e d b e f o r e the r e s u l g s $re docytpenterl. Navigation update of t h e B-IVI$, IU s t a t e u a r 4 a b l e s sitill p r e s e n t s a p r ~ b l e q ,s i n c e t h e r a d a r is mounted on t h e LM s t r u c t u r e and c o n s i d e r a b l e r a d a r a n g y l a r e r r o r s would e x i s t i f t h e s e d a t q were t r a n s f e r r e d acroBs t h e fMU (LM n a v i g a t i o n ) t o t h e IU (Saturn n a v i g a t i o n ) . It may be d e s i r a b l e t o t r a n s f e r t h e I U e s t i m a t e d s t a t e t o t h e INU and a l l o w t h e DfU t o update t h e s t a t e v a r i a b l e s i n t h e W computer and t h e n t r a n s f e r t-he updated n a v i g a t i o n a l s t a t e t o t h e I U s i n c e t h i s c a p a b i l i t y a l r e q d y e x i s t s i n t h e L,M IMU, (~~~/~orthrop) d. AAP &bf/ATM N a v i f a t i q n a l s t a t e a t O r b i t a l I n s e r t i o n (New) The working Level meeting w i t h Grumman emplayees e s t a b 1iohed c o n t a c t s f o r guidance and miss i o n a n a l y s i s . Grumman i d e n t i f i e d a need foy a LM-ATM n a v i g a t i o n a l s t a t e a t o r b i t a l i n s e r t i o n s o t h a t r a d a r a c q u i s i t i o n s t u d i e s cpuld be s t a r t e d . The LMtqTM n a v i g a t i o n a l accuracy w i l l be a s s e s s e d through t h e S - I 3 and 3-IVB b o o s t environment by s i m u l a t ing t h e IMU (M n a v i g a t i o n hardware) i n a monitor mode of o p e r a t i o n . The d u a l p l a t f o r m - a c c e l e r o m e t e r system a n a l y s i s computer program w i l l be used f o r t h i s s t u d y ? (DGG/Nor t h r o p ) C. General 1. Dynamic S t a b i l i t y of P r o p e l l a n t Tank Under Steady Load and Oscillating E x c i t a t i o n Force (New) A t h e o r e t i c a l a n a l y s i s has been conducted t o p r e d i c t t h e dynamic response of a s i m p l i f i e d model c o n s i s t i n g of a p a r t i a l l y l i q u i d f i l l e d c y l i n d e r w i t h a r i g i d f l a t bottom, a n i n t e r n a l u l l a g e p r e s s u r e , and a r i g i d mass on top. Wumerical, 3s w e l l a s e x p e r l m e n t a l , r e s u l t s have v e r i f i e d a s t r o n g coupling between t h e s h e l l , l i q u i d , and top mass. The r e s u l t s of t h i s s t u d y y i f l b e r e p o r t e d a t t h e A N S t r u c t u r a l Dynamics and A e r o e l a s t i c i t y Meeting i n A p r i l . @DS/Southwest Res. I n s t . ) �2. E v a l u a t i o n of Lumped S h e l l Analysis Methods (New) A two-task s t u d y has been conducted t o determine t h e a c c u r a c y of c e r t a i n lumped s h e l l a n a l y s i s methods. Task I was (1) t o use v a r i o u s f i n i t e element r e p r e s e n t a t i o n s t o perform a number of v i b r a t i o n a l a n a l y s e s on a c y l i n d r i c a l i s o t r o p i c s h e l l and (2) t o compare t h e r e s u l t s thus obtained w i t h known s o l u t i o n s . The a n a l y s e s were performed f o r v a r i o u s g r i d s i z e s , v a r i o u s element t y p e s , and v a r i o u s mass m a t r i c e s . The f i n a l g o a l was t o d e f i n e an optimum a n a l y s i s (one u s i n g t h e fewest degrees of freedom and t h e l e a s t computer time) t h a t would reproduce, w i t h r e a s o n a b l e a c c u r a c y , a number of t h e lowest frequency s h e l l modes. I n Task 11, f i n i t e elements were used t o perform a s e t of v i b r a t i o n a l a n a l y s e s on a g i v e n p r a c t i c a l s t r u c t u r e t o demonstrate t h e v a l i d i t y of t h e conclusions implied from Task I. The s t r u c t u r e t h a t was analyzed approximates t h e m u l t i p l e docking a d a p t e r . The b a s i c MDA s t r u c t u r e , a c y l i n d e r having a t r u n c a t e d cone a t t a c h e d t o one end, was approximated by a n e q u i v a l e n t i s o t r o p i c , homogeneous s h e l l . Two d i f f e r e n t elements and two mass m a t r i c e s were used i n t h e a n a l y s i s . The r e s u l t s of t h i s a n a l y s i s were t h e n compared w i t h r e s u l t s from a computer program known t o produce a c c u r a t e r e s u l t s f o r symmetric homogeneous s h e l l s of r e v o l u t i o n . S e l e c t i n g t h e element s t i f f n e s s and m a t r i c e s p l a y s a n important r o l e i n determining the (DDS/Martin) accuracy of t h e r e s u l t s . 3. Study of Use of Scale Models t o Determine t h e S t r u c t u r a l Dynamic C h a r a c t e r i s t i c s of Space Vehicles (Ref. October/ November 1968, p. 48) The a n a l y t i c a l development of t h e e q u i v a l e n t t r u s s r e p r e s e n t a t i o n of t h e 100-meter r e f l e c t i n g space antenna was completed. This a n a l y s i s i n d i c a t e s t h e d e f i n i t e f e a s i b i l i t y of c o n s t r u c t i n g t h e dynamic model from t h i n - w a l l tubing o r rod s t o c k i n a t r u s s con£ i g u r a t i o n s i m i l a r t o t h e p r o t o t y p e . Diagonal c r o s s - b r a c i n g of i n d i v i d u a l model bays ( r a t h e r t h a n a s i m u l a t e d r e f l e c t i n g s u r f a c e ) i s assumed i n o r d e r t o reduce t h e e f f e c t of aerodynamic damping should i t be d e s i r a b l e t o t e s t t h e model i n an ambient environment. A d e s i g n s t u d y t o e s t a b l i s h t h e optimum model s c a l e f a c t o r was i n i t i a t e d . P r e l i m i n a r y r e s u l t s of t h i s a n a l y s i s i n d i c a t e t h e f e a s i b i l i t y of c o n s t r u c t i n g t h e model from e i t h e r s t e e l o r aluminum rod s t o c k ( d i a , = 0.06 i n ) a t model s c a l e f a c t o r s a s low a s 1 / 6 0 , A l i m i t e d e f f o r t t o e s t a b l i s h c r i t e r i a f o r the model s u s pension system was conducted. No d e f i n i t e conclusions a r e y e t a v a i l a b l e . �D e f i n i t i o n of t h e r e p l i c a AAP c l u s t e r model i s c o n t i n u i n g w i t h o u t d i f f i c u l t y . The s t u d y i n d i c a t e s tfiat it w i l l b e f e a s i b l e t o c o n s t r u c t t h e MDA c y l i n d r i k a l s e c t i o n frdm one p i e c e of 6061-T6 p i p e . ~aehfning chkn+miliing processes w i i l bk used t o a c h i e v e the f i n a l thin-v&ili/weld l a n d a r e a dgpeafance. (D~s/Mdrtin) FLIGHT VIII. A. %WL!T ~ A L Y S I E DIVISXON ~ p e c i Q 1P r o j e c t s & £ i c e and S t a f f 1. F~wd-Pay1oad A hek Pligtik k v a l i i 9 t t o n w.d$khii;t ~ r o u ~ - J e a ~ l d[FEWG-P) ad prelimiiidiry U P Fd$iaiid etr&luail'dri p l k b ha3 Been d i s t r i b d k d d arid regfionkes hgve b ~ tec.eFv&. @ ~ h 3 i new d h f t 3hdi1ld GijdH b& ke&dy f o r review. THe C ~ ~ Y iI n~ EtHe FblS of h 9 ~ tfar payload3 niade the r e v i s i o d hekesdary; t h e cfiilirtnan of tHe FEWG-P m e t w i t h t h e integrkttion cont r a c t o r i n DehveF' t b d i s c l i ~ ss t & £ Guppbrt t o t h e FEWG-P, t h e p l a n comment review, and the &gent33 f o r t h e 6th. FEWG-P ineeklng scheduled fo4 February 11-12. On ~ & c & m ~21-ih5 er 1966, hk, &than inohitdl@d t h e Apollo 8 m F s d i o n from pre-18uiich through L u h a ~OrbFt I n s e r t i o n (LOIf a t t h e M i s s i o n Cdntrol Center (MCC) and Also t h e real/neaP-real-ti'me o p e r a t i o n of kH@ MSC Migsion E v a l u a t i o n Te6m ( c o u n t @ ~ p & kt to t h e MSFC &WG) i n s u p p o r t of t h e MCC and p o s t - a i s ~ i o he v a l d a t i o n , Be a l s o handled i n t e r - c e n t e r (launch v e h i c l e ) CvAluation FntePfhceb. M r ; Natfian a160 atcended two Apollo 8 f l i g h t crew d e b r i e f ings a t MCS: (a) Program &nd p r o j e c t d e b r i e f i n g on Jaduary 2, 1969. (b) Sys tems ( m i s s i o n e v a l u a t i o n ) d e b r i e f i n g on January 9-10, 1969. . ~ o n s o l i d a t e dApoll'o 8 f l i g h t crew d e b r i e f i n g n o t e s ( o u t p u t frdki t h e Technical Pr'dgram and Pro j e e t , and Sys tems D e b r i e f i n g s ) were d i 4 t r i b u t e d t o FEP meinbe?$. �B. F l i g h t E v a l u a t i o n Branch 1. Saturn I B The AS-205 p o s t f l i g h t t r a j e c t o r y r e p o r t r e c e i v e d from CCSD has been reviewed and i s b a s i c a l l y c o r r e c t . D i s t r i b u t i o n w i l l be made i n e a r l y February. 2. Saturn V a. AS-503 C' (1) (Apollo 8 ) Postflight Trajectory The p o s t f l i g h t t r a j e c t o r i e s have been d i s t r i b u t e d t o t h e v a r i o u s u s e r s . A t S-IVB f i r s t c u t o f f , t h e s p a c e - f i x e d v e l o c i t y was 0.44 m/s g r e a t e r than nominal, and t h e a l t i t u d e was 0.02 km lower t h a n nominal. This r e s u l t e d i n an o r b i t which had a n apogee 0.03 krn l e s s t h a n nominal and a p e r i g e e 0.16 km l e s s than nominal. The t r a n s l u n a r i n j e c t i o n t a r g e t i n g parameters were a l s o v e r y c l o s e t o nominal. The e c c e n t r i c i t y w a s 0.00083 l e s s than nominal, t h e i n c l i n a t i o n w a s 0.025 deg. g r e a t e r t h a n n o m i n a l , ' t h e node was 0.043 deg. g r e a t e r than nominal, and C3 was 49,631 m 2 / s 2 l e s s than nominal. A t t r a n s l u n a r i n j e c t i o n , t h e s p a c e - f i x e d v e l o c i t y was 5.23 m/s l e s s t h a n nominal, and t h e a l t i t u d e was 3.62 km h i g h e r than nominal. The s l i n g s h o t maneuver was s u c c e s s f u l l y accomplished, was placed i n a s o l a r o r b i t . and t h e S-IVB/IU (2) P o s t f l i g h t Control Analyses E v a l u a t i o n of the c o n t r o l s y s tem a c t i v i t y is e s s e n t i a l l y completed w i t h t h e e x c e p t i o n of APS p r o p e l l a n t consumption and o r b i t a l maneuvers. MDC e x p e c t s t o i n p u t t h e s e d a t a by February 3. CSM s e p a r a t i o n a n a l y s i s has n o t been completed, b u t r e c e n t i n f o r m a t i o n obtained from MSC has r e s o l v e d a l l d i s c r e p a n c i e s . To d a t e , no anomalies i n c o n t r o l system performance have been d e t e c t e d . NAR/SD has confirmed t h a t t h e 1 8 Hz o s c i l l a t i o n s e e n i n t h e c o n t r o l r a t e gyros d u r i n g t h e S - I 1 performance s h i f t w a s p r o p e r l y a t t e n u a t e d by t h e c o n t r o l £ l i t e r networks and w a s a b s e n t from t h e a c t u a t o r c u r r e n t and p o s i t i o n measurement d a t a . The magnitude sensed by t h e gyros were 10.0, .06 and 2.5 d e g / s e c peak-to-peak f o r t h e p i t c h , yaw and r o l l a x e s , r e s p e c t i v e l y . These magnitudes a r e c o n s i d e r a b l y lower t h a n sensed d u r i n g b o o s t when r a t e s of 3.2, 1.2 and 10.7 d e g / s e c were s e e n f o r f r e q u e n c i e s on t h e o r d e r of 15-35 Hz. �(3) P o s t f l i g h t Guidance Analysis The guidance aqd n a v i g a t i o n s ys tern performed v e r y s a t i s f a p f o r i l y d u r i n g a l l p e r i o d s of f l i g h t f o r which d a t a a r e a v a i l a b l e , The b o e s t n a v i g a t i o n and guidance schemes were p r o p e r l y execyted and t e r m i n a l parameters f ~ bro t 4 parking o r b i t and TLI were v e r y good. A l l t a r g e t parameters were s a t i s f a c t o r i l y achieved and o r b i t a l o p e r a t i o n s were nominal. The v e h i c l e f l e w p s l i g h t l y f l a t t e r p r o f i l e than p r e d i c t e d . A t 6-IC OECO, the v e h i c l e a l t i t u d e was l e s s than p r e d i c t e d and t h e t o t a l v e l o c i t y g r e a t e r . The r e s u l c i q g optimum f u e l usage t r a j e c t o r y determined by t h e t!@G f l i g h t pyogray wets p r e d i c t a b l e and r e s u l t e d i n s a t i s f a c t o r y end c o n d i t i o n s . The ggidaqee h@rdvataze c ~ m p ~ n e n tosp e r a t e d as deeigned. ~ r b i t a ft e l e m e t r y i n d i c a t e d gypo d r i f t s were w e l l w i t h i n s p e c i f i c a t i o n s . Telemetry from the LVaC i n d i c a t e d t h a t i n e r t i a l r e f e r ence was s t i l l being n a i n t a i n e d a f t e r 7 haurs of f l i g h t . V e l o c i t y c ~ m p a r i s ~ nwsi t h t h e f i n a l p a s t f l i g h t t r a j e c t o r y i n d i c a t e v e r y gqod cpapar$sone f o r t h e b o o s t t a p a r k i ~ go r b i t t r a j e c t o r y . The comparisons a r e ~ e l a t i v e l ygosd f o r t h e a e ~ o n dS-IVB burn. The d i f f e r e n ~ eprobably r e s u l t s more from t r a j e c t o r y d a t a than t h e LVnCi Rowewer, campanent d i f f e $ a n c e a do 9esulF from a prpgrwmed v e p t i n g p r o f i l e used d u r i n g p a r k i n g o q b l t , The tatal v e l o c i t y change d u r i n g second S-IVB burn as computed by t h e LVQG was 2.2 mdsec g r e a t e r t h a n s h o r n by t h e p o s t f l i g h t t r a j e c t o r y . The v e l a c i t y change as measured by t h e ST-124-M-3 p l a t f o r m system w4s w i t h t n 0.05 m/sec of t h e o p e r a t i o n a l t r a j e c t o r y v a l u e f o r t h e second S-TVB hu'rq mode. ( 4 ) P o s t f l i g h t C l u s t e r e d Engine P r o p u l s i o n Analysis The S-IC c l u s t e r e d engine p r o p u l s i o n a n a l y s i s was made by Boeing H u n t s v i l l e (TBC) u s i n g t h e i r r e c e n t l y developed g r a p h i c s d i s p l a y c g p a b i l i t y . The g r a p h i c d i s p l a y has proved t o be a v e r y u s e f u l t o o l t o speed t h e p r o p u l s i o n a n a l y s i s . It has enabled TBC t o meet t h e i r d e l i v e r y schedule although the f i r s t propulsion reconstruction d a t a tape from R-P&VE had erroneous d a t a . A p r e l i m i n a r y d r a f t of t h e f i n a l r e s u l t s of t h e i r a n a l y s i s has been r e c e i v e d ; t h e f i n a l r e p o r t w i l l be p u b l i s h e d by 35 days a f t e r launch. �(1) Emergency D e t e c t i o n System Analysis The TBC Document No. ~5-15555-4B, "Saturn V Launch Vehicle Emergency D e t e c t i o n Sys tem A n a l y s i s , SA-504," r e c e i v e d January 13, 1969, has been reviewed. Comments were s e n t t o TBC, and t h e r e v i s e d document should be d i s t r i b u t e d i n e a r l y February. The F l i g h t Mechanics Panel Document No. 69-FMP-1, "AS-504 Mission D , Apollo 9, Emergency D e t e c t i o n System (EDS) and F l i g h t Dynamics L i m i t s , ' ' i s b e i n g reviewed. D i s t r i b u t i o n i s planned f o r e a r l y February. (2) Dynamics Analysis and Wind Limits The dynamics a n a l y s i s document was d e l i v e r e d by TBC on January 30, 1969. The i n f l i g h t wind l i m i t s a r e p r e l i m i n a r y ; updated ones based on t h e l a t e s t t r a j e c t o r y and s t r u c t u r a l d a t a should be d i s t r i b u t e d i n e a r l y February. (3) Abort and A l t e r n a t e Mission Analysis The S a t u r n AS-504 Launch Vehicle O p e r a t i o n a l Abort and A l t e r n a t e Mission T r a j e c t o r y document was d e l i v e r e d January 30, 1969, on s c h e d u l e . The document, now being reviewed, should be ready f o r d i s t r i b u t i o n i n February. No S-IVB s t a g e PU f a i l u r e a n a l y s i s was performed d u r i n g f i r s t burn s i n c e e a r t h parking o r b i t (EPO) can b e a t t a i n e d w i t h a PU f a i l u r e t o any p o s i t i o n . This b e i n g a "D" m i s s i o n , i t was f e l t t h a t a n o u t - o f - o r b i t S-IVB PU f a i l u r e a n a l y s i s w a s n o t n e c e s s a r y . Also, EPO can b e a t t a i n e d f o r S - I 1 s t a g e mT f a i l u r e t o any p o s i t i o n . On AS-203, w i t h a 30 low performing v e h i c l e and a Z-accelerometer f a i l u r e b e f o r e 280 seconds, t h e S-IVB s t a g e f a i l e d t o a c h i e v e a 75 n.m. p e r i g e e . For AS-504, t h e S-IVB s t a g e can a c h i e v e a 75 n.m. p e r i g e e f o r a Z-accelerometer f a i l u r e a t any time. On AS-503, w i t h a 30 h i g h performing v e h i c l e and a n X-accelerometer f a i l u r e b e f o r e 80 seconds, t h e S-IVB s t a g e f a i l e d t o a c h i e v e a 75 n.m. p e r i g e e . For AS-504, w i t h a 30 low performing v e h i c l e and a n X-accelerometer f a i l u r e b e f o r e 60 seconds, t h e S-IVB s t a g e f a i l s t o a c h i e v e a 75 n.m. parking o r b i t . J Abort and a l t e r n a t e m i s s i o n p r e s e t t i n g s f o r t h e LVDC f l i g h t program were checked and s u p p l i e d t o R-ASTR a s scheduled. �c. General (1) 6?D p a j e c t q r y C a p a b i l i t y Development S i n c e t h e dgcfsj.on w a s made t o g o t o a s i n g l e 6-D t r a j s c c p ~ ys i p u l a t i o n p r o g y p on t h i Upivac 1108 f o r u s e w i t h i n t h e d i v i s i ~ p ,puch p l a l ~ n i n gand o r g a n i z a t $ o n have been accpmplished. The gchedule goy t h e n y j o r m i l e s t p n e ~is shown Date - Capab il i f y . -. '1°C " o p e r a f i o n a l t r a j e g f ~ f@9-505) ~ Reg$- tra j e c t ~ p ySuPPoyt: (48-505) PSM p i e d t o OT degk February 15 March 15 April 1 The a t p t u ~pg t h e a p e r a t i o n a l t r a j e c t o r y is a s follows: (a) A l t h ~ u g hR-FOMP p e r s q n n e l have worked v e r y hard t o c o n v e r t t h e p r e s e n t ~ A A Mdeck fit h e Upivac 1108, v e r y l i t t l e p r o g r e s s ha9 been made thus f a r . The d i f f i c u l t i g s a r e w i t h t h e systetp and a r e somewhat random. Thg encqprag$n& a s g e F t of t h i s is t h e e x c e l l e n t t u r n around pn t h e Urliva5: 1108. ( Chepko~kpf t h e IGM mqdule f o r S _ I ~ b u is~ ~ ~ n f i n u j npr, g t h e IBg 7994 slM c q p l e t e thrqygh $-IVB r e i g p i t i a n . To p s q i s t ip t p i s chqpkqyFI rgry@!4 as f o r fqcpyd prqbiems, ~ ~ ' I c $ I r a u t i s e whiph can r)m indepegdeptly of php 6-0 t r a j e c t o r y ' brogram i s being prepared. (c) Berssnnel have been a s s i g n e d t o e s t a b l i s h she c a p a b i l i t y t o a c c e p t a P&VE p r o p u l s i o n t a p e and t o o u t p u t a B7 t a p e , and t h e work w i l l ' q o o n begin. The d e t a i l e d t a s k s r e q u i r e d f o r t h e o t h e r m i l e s t o p e s have been d e f i n e d , and p e r s o n n e l have been a s s i g n e d . Considera b l e planning must be done i n t h e do~um-entationand d a t a c o o r d i n a t i o n prqcpdures. (2) S-IC Engine-Out Chi-Breeze Schedule The AS-504 c h i - f r e e z e s c h e d u l e f o r a n S-I€ s t a g e engine f a i l ~ r ewas n o t p r o p e r l y implemented i n t h e Launch Vehicle D i p j F a l Computer (LVDC), I f a n engine were t o f a i l b e f o r e T1 14 secs., t h e LVDC would compute t h e l e n g t h of c h i - f r e e z e based on a T1 14-secpnd englpe f a i l u r e . This could r e s u l t i n t h e c h i - f r e e z e d u r a t i o n being ~ e a y by ~ das much as 9.6 geconda. A s t q d y was made t o d e t e r q i n e t h e e f f e c t of t h e s h o r t e r c h i - f r e e z e on e a r l y F-1 engine f a i l u r e s . For ~ p g $ p a lwinds, b o t h t h e A S ; ~ O ~and AS7505 v e h i c l e s would l o s e c o n t r o l 4ufCng S-IC pqwered f l i g G t f o r a lower c o n t r o l engine f a i l u r e b e f o r e + + �approximately T1 + 6 seconds. The most obvious s o l u t i o n t o t h e c o n t r o l problem would be t o change t h e LVDC l o g i c and corresponding hardware t o p r o p e r l y implement t h e p r e s e n t c h i - f r e e z e schedule. However, because of l a c k of time, t h i s change could n o t be made on t h e AS-504 and AS-505 v e h i c l e s w i t h o u t a d e l a y i n t h e launch s c h e d u l e s . An a l t e r n a t e s o l u t i o n , a l t h o u g h i t i s n o t as d e s i r a b l e , would be t o change t h e c h i - f r e e z e schedule. It has been v e r i f i e d t h a t a'60-second c h i - f r e e z e d u r a t i o n , f o r a n F-1 engine f a i l u r e b e f o r e TI 14 seconds, would s o l v e t h e cont r o l problem. This s o l u t i o n has been implemented on t h e AS-505, and is now scheduled f o r t h e AS-504. A memorandum recommending that: t h e LVDC l o g i c and a s s o c i a t e d hardware be modified on t h e AS-506 and subsequent v e h i c l e s t o permit t h e use of t h e d e s i r e d c h i - f r e e z e s c h e d u l e , has been s e n t t o R-ASTR-NG. + (3) Navigation Update A n a l y s i s The Boeing document No. 5-9600-H-160, "SSR-216, Navigation Update C a p a b i l i t y Checkout," December 16, 1968, w a s r e c e i v e d . S i n c e t h i s document is v e r y l e n g t h y , a summary (Memo No. R-AERO-FF-1-69) i s being d i s t r i b u t e d . The n a v i g a t i o n update a n a l y s i s i n d i c a t e s t h a t l u n a r l a n d i n g m i s s i o n f a i l u r e s a r e reduced by performing a n update i n e a r t h p a r k i n g o r b i t . Assuming t h e "present" (45 m/s) midcourse AV budget, 3200 f a i l u r e s (per m i l l i o n f l i g h t s ) a r e reduced t o 2500. I f t h e "proposed" (18 m / ~ )budget i s used, 15400 f a i l u r e s a r e reduced t o 3360 failures. S e v e r a l items concerning n a v i g a t i o n update s t i l l need t o be i n v e s t i g a t e d . One i s t h e e f f e c t of manual c u t o f f s t o p r e v e n t e x c e s s i v e overspeeds. Another is t o determine t h e AV budget r e q u i r e d t o reduce f a i l u r e s t o a more d e s i r a b l e l e v e l . (4) P r o p u l s i o n S i m u l a t i o n Module (Operations Research, I n c o r p o r a t e d (ORI) ) S e v e r a l m o d i f i c a t i o n s have been made t o t h e SPED- PSM computer program t o enhance i t s u t i l i t y . ( a ) The i n f l u e n c e c o e f f i c i e n t model was a l t e r e d s o t h a t Rocketdyne i n f l u e n c e c o e f f i c i e n t s f o r PU v a l v e a n g l e , m i x t u r e r a t i o , and c h a r a c t e r i s t i c v e l o c i t y c o r r e c t i o n could b e used d i r e c t l y . (b) The i n f l u e n c e c o e f f i c i e n t model was provided w i t h a n independent v a r i a b l e f o r use i n performing p e r t u r b a t i o n a n d / o r dispersion analyses. �(c) The engine model was provided w i t h a b i a s and s c a l e f a c t o r a r r a y t o a i d i n compensating f o r n o n l i n e a r i t i e s and d a t a incompatibil i t i e s . A l l of t h e s e modifications have been programmed, checked o u t , and documented. (5) S t u d i e s i n the Theory and A p p l i c a t i o n of Kalman F i l t e r i n g Two r e p o r t s have r e s u l t e d from a c o n t r a c t w i t h t h e Univac Federal Systems D i v i s i o n of Sperry Rand. The f i r s t r e p o r t , " I n t r o d u c t i o n t o Kalman F i l t e r i n g , " is a survey of the t h e o r e t i c a l developments l e a d i n g t o Gauss's l e a s t s q u a r e s , Markov's minimum v a r i a n c e s t a t i s t i c a l e s t i m a t i o n theory, t h e Wiener f i l t e r , and t o t h e u n i f i e d e x t e n s i o n t o t h s Kalman f i l t e r , A step-by-step computational procedure f o r the Kalman f i l t e r is developed w i t h s e v e r a l s p e c i f i c a p p l i c a t i o n s given. The r e p o r t includes an exten'sive l i s t of r e f e r e n c e s . The second r e p o r t , "Survey of E r r o r Sources f o r Estimates i n Kalman ~ i l t e r i n g , " i d e n t i f i e s t h e causes and e f f e c t 8 t h a t lead t o v a r i o u s e s t i m a t e e r r o r s and d i s c u s s e s t h e v a r i o u s methods t h a t have been proposed f o r t h e i r treatment. These methods a r e derived i n d e t a i l using a n o t a t i o n comp a t i b l e w i t h t h e former r e p o r t . The problem of d a t a s a t u r a t i o n is explored, and s e v e r a l approaches f o r salutian are developed. C. Tracking and O r b i t a l Analysis Branch 1. Saturn V AS-503 C t Mission a. (1) A s h i p - t r a c k i n g and communications a n a l y s i s was i t e r a t e d s e v e r a l times b e f o r e a f i n a l s e t of coordinates f o r t h e s h i p s The f i n a l a n a l y s i s was documented i n memorandum was e s t a b l i s h e d R-A.ERO-FT-50-68. . (2) The S-IVB s t a g e was s u c c e s s f u l l y perturbed by l u n a r g r a v i t y t o a c h i e v e a h e l i o c e n t r i c o r b i t . This l u n a r g r a v i t y pert u r b a t i o n caused a s l i n g s h o t e f f e c t by adding s u f f i c i e n t v e l o c i t y t o the S-IVB s t a g e t o achieve a n e a r t h escape v e l o c i t y (C3 w i t h r e s p e c t t o the e a r t h > 0). O r b i t parameters of t h e s t a g e a t p e r i c y n t h i o n (lunar c l o s e approach) a r e a s follows: �D i s t a n c e t o c e n t e r of moon Distance t o lunar s u r f a c e O r b i t i n c l i n a t i o n t o l u n a r equator D e c l i n a t i o n o r l a t i t u d e of c l o s e approach subpoint* Longitude of c l o s e approach s u b p o i n t (pos e a s t ) * Approximate time of c l o s e approach Dec, 24, 1968 3000 km 1262 km 44-56" 0.4" 79.6" 10: 50 U.T. These parameters a r e based on a Goddard Space F l i g h t Center v e c t o r f o r t h e S-IVB s t a g e on ~ e c e m b e r22 a t 0100 U.T. This v e c t o r was determined u s i n g t h e b e s t t r a c k i n g i n f o r m a t i o n a v a i l a b l e (Unified S-Band t r a c k i n g of t h e S-IVB s t a g e from s t a g e p a s s i v a t i o n u n t i l l o s s of CCS s i g n a l due t o b a t t e r y l i f e t i m e t e r m i n a t i o n ) . The h e l i o c e n t r i c o r b i t of t h e S-IVB s t a g e is a s follows : Semimajor a x i s Aphel i o n Perihelion Eccentricity I n c l i n a t i o n t o e q u a t o r i a l plane Period V e l o c i t y a t aphelion** V e l o c i t y a t peri2Elion** Average v e l o c i t y " " b. AS-504 "D" 1.428 x l o 8 km 1.4774 x lo8 km 1.3795 x lo8 km 0.03427 23.47" 340.8 days 29.45 kmlsec 31.54 km/sec 30.5 km/sec Mission ( I ) The t r a c k i n g and communications a n a l y s i s has been completed and d i s t r i b u t e d . +\ (2) Magnetic t a p e s of l o o k a n g l e and o t h e r s u r v e i l l a n c e d a t a have been t r a n s m i t t e d t o TBC, MSC, IBM, MDC, NAA, and John Hopkins U n i v e r s i t y . These u s e r s a r e s u p p o r t i n g R-ASTR i n t h e i r a n a l y s e s . *Referenced t o a moon-centered c o o r d i n a t e system d e f i n e d a s : X-axis p o i n t s from moon c e n t e r t o e a r t h c e n t e r (moons z e r o l o n g i tude l i n e ) . z - a x i s p a r a l l e l t o e a r t h a x i s of r o t a t i o n (through North P o l e ) . Y-axis forms right-handed system. **These v e l o c i t i e s a r e w i t h r e s p e c t t o t h e s u n and a r e v e r y s i m i l a r t o t h e v e l o c i t i e s of t h e e a r t h about t h e sun s i n c e t h e S-IVB'S o r b i t and the earth's o r b i t a r e very similar. �( 3 ) A memorandum on t r a c k i n g and cotmnu~ications a c q u i s it i o n and l o s s d a t a f o r a l t e r n a t e m i s s i o n s of t h e launch v e h i c l e has been prepared. ' ( 4 ) ~ n a t y s i shhd been performed t o i n s u r e nb S-IVB impzict, of t h e mdon, A 1 1 d2itei, laurfch times, and azimukh windows i n d i c a t e t h a t the S-IVB W i l l n o t impact t h e inobn on a ndminal m i s s i o n , For t h e contingency mi9sion With afily bne burn, the S-IVB does pass i n t h e v i c i n i t y of t h e &on, b u t a g a i n no impaktii werk i d e n t i f i & d , t h e c l o s e s t approach t o t h & boon bking approximately 5b,00O k i l o m e t e r s . (1) an g'sR hds t h e n sFg6bd w i t h TBC Fd p r b t i d e p r o p & r a t t i t u d e s and tbh &V r e q h i i e d fur t h e &t$g& t o s l i & e l i t l t , t h e htbon. $i-&linikridky ?e&bik8 Wgre $ i \ f k h t b k-Am# &fid R-P&& t d hfibblb thzSit a n a l y s e s t o coritihiie. ?hes& prkiihifiai-jr fjardihgterg inf&e' d = l l b O akid nv = 40 rntl!!ec. A f 8 a k i b i l i t y dtudy vaB &rforrned dri t h e p 6 d s i b i l i t y of k o n t t o l l i n g t h e g a r t h r e e n t r y of t h e s - W ~s t a g e fkom a 100 n.thi. o r b i t . The s t u d y d & ~ u m e dt h e d& on a l d a r m i s s i o n s e p a r a t e d f r m t h e , S - ~ i T f f i n e a r t h b r l i i t ; and thS drage e ~ d i dBe r e e n t e r e d b$ & i t h e r f e i g n i t i n g t h e S-IVB o r By a cold dd&p 8f tHe p f ~ h 8 1 . f a n t s d ~ r e l f h i n a ri n~ v e s t i gatioris show k h d t e i t h e r dead3 k b b i d be ddkd t o r e b h t e k khe S-IVB i n t b an ocean a r e a t o minimize t h e hdsayds of o r b i t a l d e b r i s . However, t h e irripact f o o t p r i n t could be g r e a t l y reduced by r e i g f i i t f n g t h e s t a g e and a p p l y i n g a much l a r g e r e q u i v a i e n t retro-AV. Orbftirl decay and l i f e t i t t r e s f o r v a r i o u s f l i g h t a b o r t s and e a r l y f l i g h t t e r m i n a t i o n s on t h e AAP m i s s i o n a r e being i n v e s t i g a t e d . These s t u d i e s , t o b e used t a dete*mine madimum d e l a y s which could occur ahd s t i l l complete t h e b a s i c c o r e missitjn, i n c l u d e u s i n g only a nominal decay w i t h b o o s t c a p a b i l i t i e s of t h e fdllow-on CSM~s. R e s u l t s of t h e s e deeay and l i f e t i m e a n a l y s e s w i l l be documented by memorandum. �D. F l i g h t Mechanics Branch 1. Saturn V a. AS-503 C' Mission (1) Operational T r a j e c t o r y : The f i n a l p u b l i c a t i o n of t h e Boeing Company's Operational T r a j e c t o r y f o r ~ e c e m b e r l ~ a n u a rwas y received and d i s t r i b u t e d approximately 10 days before launch. Although t o o l a t e t o s e r v e a s a g e n e r a l r e f e r e n c e f o r t h e Apollo 8 mission, i t w i l l be t h e b a s e l i n e a n a l y s i s f o r subsequent lunar mission o p e r a t i o n a l trajectories. (2) Targeting: The a c t u a l r e s u l t s of t h e Apollo 8 t r a n s l u n a r i n j e c t i o n (TLI) powered f l i g h t , with t h e p r o j e c t e d required midcourse of approximately 6 f e e t per second computed i n r e a l time by MSFN (Manned S p a c e f l i g h t Network), has proven t h e Saturn V launch v e h i c l e s y s tem c a p a b i l i t y t o perform t h e l u n a r mission. I n p a r t i c u l a r , t h e hypers u r f a c e concept, t h e mode of t a r g e t i n g ( i . e . , g e n e r a t i o n of t h e numerical c u t o f f c r i t e r i a and t h e IGM s t e e r i n g concept and implementation) and t h e innumerable s i m u l a t i o n models a r e no longer s u b j e c t t o t h e q u e s t i o n of whether a b a s i c flaw e x i s t s . However, t h e p o t e n t i a l of unknown cons t r a i n t s , e s p e c i a l l y i n t h e t a r g e t i n g a r e a , s t i l l e x i s t s . The r e a l l e s s o n from t h i s mission a n a l y s i s i s t h e establishment of "for r e a l " procedures of g e n e r a t i o n and v e r i f i c a t i o n . Basic flaws d i d e x i s t here i n t h e c o n t r a c t o r check procedures, a s exampled by t h e 17-second e r r o r i n e s t a b l i s h i n g t h e Apollo 8 launch window. Steps a r e being taken t o expose t h e p o t e n t i a l t a r g e t i n g t r o u b l e a r e a s (i.e., l u n a r d e c l i n a t i o n s g r e a t e r than t h e launch l a t i t u d e and h i g h l u n a r c l o s e approach d i s t a n c e s ) and t o produca procedures which w i l l p o s i t i v e l y check t h e t a r g e t i n g a c t i v i t i e s . On t h i s mission, 15 d a i l y windows were t a r g e t e d . (3) The E a s t e r n T e s t Range placed t h e a d d i t i o n a l requirement of many contingency t r a j e c t o r y s i m u l a t i o n s b e f o r e a f l i g h t waiver was g r a n t e d . Again, being t h e f i r s t Apollo v a r i a b l e azimuth launch, and a l s o p o t e n t i a l l y t h e most s o u t h e r l y f l i g h t azimuth, t h e range s a f e t y a n a l y s e s f o r t h i s mission should s e r v e a s b a s e l i n e a n a l y s i s f o r a l l Saturn V launches i n t h e 72 t o 108 degree f l i g h t azimuth s e c t o r . ( 4 ) The low payload requirement f o r t h i s mission reduced t h e s i g n i f i c a n c e of t h e f l i g h t performance r e s e r v e requirement g e n e r a t i o n , except as a b a s e l i n e f o r f u t u r e l u n a r missions. The midcourse requirement envelopewas of more concern and i n t e r e s t and w i l l probably s e r v e a s t h e b a s e l i n e f o r f u t u r e Apollo lunar missions. �(5) Real Time T r a j e c t g r y Support: While the m i s s i o n experienced no contingency'sl't'uatcon which might h u l y e x e r c i s e t h e assessment c a p a b i l i t y of f h e 1n-f l $ h t T r a j e c t o r y Teay, t h e time l i n e of a c t i v i t y was extremely smooth. --y--* (6) Slj. g h a t . The concept and implementatioq of t h e s l i n g s h o t methpd Q£ S - I n i s p b s a l was s u c ~ e s s f u l l ydemonstrated. Reasonably r g l i a b l e gigpoqal of t h e S-SVE s t a g e should npxq g x i s t f o r f u t u r e l u n a r mieqionq. ( 7 ) F l i p h g E e r f o r q n c e f n ~ e n t i v e : F l i g h t performance i n c e n t i v e c r i t e r i a were'es'r'blY$bed $or t h ' k X $ - 1 C (Boeing) , S-IVB (McDonnell Douglas], an4 IU [ I n t e r n g f $ o n a l Business Machines). C o ~ t ~ a c t u na el g p t i a Cipns between TO qpd Boaiqq did n a t culmipate i n a f l i g h t p e y f a r w n c e agreement f o r migsioq, It wap n e c e s s a r y , dqe t o t h e v a y t q b l p a z i q u t h f e a t u r e , Po e~t a k l i g h q '!pop t ~ l a u n c ho p e r g t i o n a l t r a j e c ~ o y y l ' i n o r d e r t o have a b a s a l i q e f o r compariqqn. . A O ~ 5 0 4"D" Misgion ( 1 ) C&eggti~qg$ T r a j e p t q ~ y : The docupeqped a n a l y s i s r ~f +aunch pad from was r e l e a s e d on 16 ~ ~ c e m 6 ; r19q"d". ~ u b ~ e q b e n tcharlge " R J I go "A" pn Coqplex 39, p i u s an p p d g ~ gpf p ~ ~ p u l s i ogata n has resglted i a a t r a j e c t o r y y p d ~ f e . Th&g ~ 5- 1 1ka rplaased a p p r ~ q & ~ t e ! y 3 0 J3;jnuqry, a i t h o p g h t h e b a s i c a n a l y s i s i n Ehe e a s / b e g docwnegt w L ) l s t i l l be vaf i d . i( (2) Digpgrsioq Anqlysipr This docqment i s n e a r l y ready f o r d is t r i b u t t o p m c = 6 $ r g i p problem e x i s t g f o r e i t h e r c ~ m p l e t i o nof t h e t h r e e primary S - I D s t a g p burns t o egcape o r t h e two contiqgency 9-IVB s t a g e burns t o escape, (3) S e Safety: The range s a f e t y analys'es f ~ t rh i s v e h i c l e have been publ%sKe,d ( k i d - ~ a n u a ~ y )a,l o p g w i t h s e v e r a l a d d i t i o n a l cages r e q y e ~ t e dby t h e E a s f e r n T e s t Raqge. No a d d i t i p n a l e f f o r t i s a n r t c i p a t e d r e s u l t i n g f r w t h e chang,e i n launch pads. (4) Guj-dance P r e s e t r i n g s : The guidance p r e s e t t i n g s were t r a n s m i t t e d t o ~ s t f i b n i c b oh 2 f GbvGmber 1968. A s is t y p i c a l w i t h t h i ~d e l i v e r y , i p s u f f i c i e n t time was a v a $ l a b l e t o v e r i f y them inhouse prior t o transmittal. S e v e r a l follow-up meetings were held t o c l a r i f y d e f i n i t i o n s and, i n some c a s e s , t o modify some numbers. �c. AS-505 "F" Mission (1) O p e r a t i o n a l T r a j e c t o r y : An i n t e r i m r e l e a s e of t h e o p e r a t i o n a l t r a j e c t o r y document is due on February 11, 1969. This w i l l c o n t a i n d a t a o n l y f o r t h e f i r s t 4 d a i l y windows i n May. The f i n a l r e l e a s e , due March 15, 1969, w i l l be comprehensive f o r t h e 6-day windows of b o t h May and June. The J u l y o p p o r t u n i t y , n o t y e t d e f i n e d , w i l l b e worked on a two-month turnaround b a s i s o n l y i f a May launch does n o t occur. (2) T a r g e t i n g : T a r g e t i n g i s complete and d a t a t r a n s m i t t e d f o r t h e 17 May window, o n l y , w i t h t h r e e a d d i t i o n a l days of May t o be d e l i v e r e d on 27 January. The remainder of May and June a r e due February 14. The nominal midcourse c o r r e c t i o n r e q u i r e d i s i n s i g n i f i c a n t . Note t h a t S p a c e c r a f t Reaction Control System (RCS) margin f o r t h i s m i s s i o n i s much more c o n s t r a i n e d r e l a t i v e t o Apollo 8 a s a r e s u l t of t h e presence of t h e LM. (3) Guidance P r e s e t t i n g s : Guidance p r e s e t t i n g s were t r a n s m i t t e d ( l a u n c h d a t e independent) t o A s t r i o n i c s on January 23, 1969, i n accordance w i t h s c h e d u l e requirements. 2. AAP CCSD has been a u t h o r i z e d t o proceed on range s a f e t y a n a l y s e s i n s u p p o r t of m i s s i o n a n a l y s e s f o r AAP-1, -2, and - 4 . The b a s i c g o a l is t o a c h i e v e p r e l i m i n a r y range s a f e t y approval f o r t h e s e m i s s i o n s by mid-summer . 3. Quick Response T a r g e t i n g Program (QRTP) Conversion t o t h e Univac 1108 computer system h a s been achieved f o r t h e midcourse c o r r e c t i o n r o u t i n e of t h i s program. The t a r g e t i n g r o u t i n e w i l l be checked n e x t . If t h i s program i s o p e r a t i o n a l i n time, t h e "F" m i s s i o n t a r g e t i n g f o r t h e J u l y o p p o r t u n i t y w i l l be attempted a s b o t h a checkout and a l s o a s o p e r a t i o n a l s u p p o r t i n t h e e v e n t of a launch s l i p . �BIBLLOGRAPHY 1. NASA TN D-4963, "The I n f l u e n t i a l Aspects Of Atmospheric D i s t u r b a n c e s on Space Vehicle Des i g n Us i n g S t a t i s t i c a l Approaches f o r A n a l y s i s , I t January 1969. 2. A U A Paper No. 69-58, "A Study of S a t u r n AS-502 Coupling L o n g i t u d i n a l S t r u c t u r a l V i b r a t i o n and L a t e r a l Bending Response D~rlttlgBoost," p r e s e n t e d a t A W 7 t h A@rospaice S c i e n c e s Meeting, New York, New York, J a n u a r y 20-22, 1969. 3. TR-795-8-420, "Dynamic A n a l y s i s of ~ k n g e dF l e x i b l e Space V e h i c l e s , " C o n t r a c t MdS8-20082, M o r t r o n i c l l R u h t s v i l l e . 4. TR-795-8-498, "An I n v e s t i g a t i o n of S a t u r n VIS-IC S t a g e Coupled Long Feud i n a l i3 t r u c t u r d l V i b r a t i o n whd L a t e r a l Bending Response During Boost Ff i g h t , " Mortlronfcs/Humltaville, 5. A E R 0 - ~ ~ - 1 4 4 - 6 8 ,"Saturn V O f f i c i a l Dynamics Data," December 23, 1968. 6. R-AERo-DD-~~~-& ttljynopsis &, of POGO A c t i v i t i e s 7. R-AERO-DD-148, " ~ f f i c i a lDynamic Data f o r AS-504, Mission "D", A f t e r Payload S e p a r a t i o n , " J a n u a r y 7, 1969. 8. R-AERO-DD-1, " U P S t r u e t u l a l DynarrllLci~Data," J a n u a r y 24, 1969. 9, 8-AERO-DD-2, "Technical E v a l u a t i o n of Propo6als Received i n Response Advanced Subs t r u e t u r ing ~ e c h n i ~ u .eI f k t o RFQ DCN 1-9-75-10045 10. R-AERO-DCC-12-68, " P r e l i m i n a r y Rigid Body C o n t r o l Responses f o r t h e S a t u r n IB, AAP-2 M i s s i o n , f o r M r c h 1 and Near-IECO," Dec. 1 8 , 1968, 11. R-AERO-DCC-~~-~S, "Wind Tapes f o r GPS High Speed Analog Computer," December 1 0 , 1968. 12. R-AERO-DCC-14-68, 1968. ,It December 11, 1968. S-IVB - "Ag-503 C ' M i s s i o n , Vehicle S t a b i l i t y , " December 1 8 , I 13. IN-AERO-68-7, "Discuss i o n of Manual C o n t r o l Problems , I t DecesnbG 27, 1968, James H. Colmon. 14. IN-AERO-69-1, "Aerodynamic Design and C a l i b r a t i o n of t h e MSFC Thermal Cobd Flow Duct," J a n u a r y 9, 1969, K , D, Acoustic J e t F a c i l i t y Johns t o n , W-AERO-A, and W. C. Tidmore , Nor throp-Nor t r o n i c s H u n t s v i l l e 15. - TM X-53813, "The Use of a Ground-Baged MultPple-Beam D e t e c t o r i n Crossed-Beam Atmospheric Experimentation," J a n u a r y 30, 1969, W. H. Heybey. . �APPROVAL L: /&<./>,+.A, E . D. G e i s s l e r D i r e c t o r , Aero-Astrodynamics Laboratory DISTRIBUTION R-AERO-DIR Dr. G e i s s l e r M r . Jean Mr. B u t l e r R-AERO-R Mr. B e a n ( 4 ) Mrs. H i g h t o w e r Mrs. P e t t u s R-AERO-T Mr. M u r p h r e e Mr. C u m m i n g s Dr. Heybey Mr. J a n d e b e u r Dr. K r a u s e Mr. N a t h a n Mr. Few M r . von P u t t k a m e r R-AERO-P R-AERO-D R-AERO-A R-AERO-G R-AERO-Y R-AERO- F R-AERO-X PAO, M r . K u r t z R-DIR, MS-H, I-V-P, Mr. W e i d n e r M i s s J e r r e l l (3) Mr. P r i c e � Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000049 Title A name given to the resource "Aero-Astrodynamics Laboratory Bimonthly Progress Report: December 1968 - January 1969." Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1969-02-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn Project (U.S.) NASA space programs Project management Type The nature or genre of the resource Progress reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 30, Folder 20 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000027_000050 https://digitalprojects.uah.edu/files/original/20/1153/spc_stnv_000069.pdf 6c92c6333b33c9db43bdc6e18470ad6d PDF Text Text Reproduced for N A S A by the NASA Scientific and Technical Information Facility -..-"-./ FFNo 474 S e p t 65 ��Wl-*.--~.-I^IYi Y-rr*- & ,. -1 * ' A ' * . ----+. d . . # . " * * LI Distribution Must Be Authorized . I I This document will not be indexed or announced in Scientific and Technical Aerospace Reports. The Document has received partial Descriptive cataloging only. i i , 1 i i I I I I i1 I 1 I I Available to NASA Offices and NASA Centers Only. 'No 7 9 3 . July 1966 I 1 �APOLLO INTERFACE CONTROL DOCUMENT LOG ENGINEERING ADPS RECORDS U N I T DOCUMENTATION CONTROL SECTION ENGINEERIKG DOCUMENTATION BRANCH VEHICLE SYSTEMS D I V I S I O N PROPULSION AND VEHICLE ENGINEERING LABORATORY GEORGE C. MARSHALL SPACE FLIGHT (=ENTER �APOLU) INTERFACE CONTROL DOCUMENT UX; ABSTRACT T h i s l o g i s p u b l i s h e d f o r N a t i o n a l Aeronautics and Space A d m i n i s t r a t i o n H e a d q u a r t e r s , Washingtor,, D. C. by t h e George C. M a r s h a l l Space F l i g h t C e n t e r and i s a l i s t i n g , i n alpha-numeric sequence by e f f e c t i v i t y of Apollo I n t e r f a c e documents and r e v i s i o n s r e l e a s e d and s c h e d u l e d t o b e r e l e a s e d f o r S a t u r n ZB, and S a t u r n V v e h i c l e s w i t h r e s p e c t t o Apollo. The i n f o r m a t i o n l i s t e d i n t h i s r e p o r t i s o b t a i n e d from I n t e r f a c e C c n t r o l Document Log I n p u t Fo,rms (MSFC Form 2053) s u b m i t t e d t o M a r s h a l l Space F l i g h t C e n t e r by t h e r e s p o n s i b l e I n t e r f a c e Panels. T h i s l o g i s p u b l i s h e d monthly, r e f l e c t i n g a l l d a t a r e l e a s e d p r i o r t o t h e 2 5 t h day of t h e p r e c e d i n g month, and s u p e r s e d e s a l l p r e v i o u s e d i t i o n s . IAOl �CHG - DS' - Change: A s t e r i s k (*) i n d i c a t e s change from p r e v i o u s e n t r y . S i n g l e p l u b (+) i n d i c a t e s s c h e d u l e d r e l e a s e d a t e i s w i t h i n 60 d a y s o f b e i n g d e l i n q u e n t . Double p l u s (-I+)i n d i c a t e s s c h e d u l e d r e l e a s e d a t e i s w i t h i n 30 d a y s o f b e i n g d e l i n q u e n t . T r i p l e p l u s (ftF) i n d i c a t e s s c h e d u l e d r e l e a s e d a t e i s d e l i n q u e n t . L e t t e r i n d i c a t i n g s i z e o f document. DOCUMENT NUMBER REVISION NOTICE Numerical i d e n t i f i c a t i o n o f document. Numerical i d e n t i f i c a t i o n o f I n t e r f a c e R e v i s i o n N o t i c e . DOC REV The r e v i s i o n l e t t e r o f a document. Dash (-) i n d i c a t e s no r e v i s i o n . 1X)CUMENT TITLE OR CCBD NUMBER F u l l t i t l e o f document may b e a b b r e v i a t e d a n d / o r t h e C o n f i g u r a t i o n C o n t r o l Board D i r e c t i v e number. SCHED REL DATE D a t e document (and e a c h r e v i s i o n ) i s s c h e d u l e d t o b e r e l e a s e d by t h e P a n e l f o r t e c h n i c a l use. ACTUAL REL DATE D a t e document i s r e l e a s e d b y t h e P a n e l t o t h e R e p o s i t o r y . PANEL CODE I n t e r f a c e P a n e l r e s p o n s i b l e f o r document. INTERFACE AREA OR CEI NUMBER A coded n u m e r i c a l i d e n t i f i c a t i o n o f t h e I n t e r f a c e Area o r t h e C o n t r a c t End I t e m number. - PREPARING CENTER ACTIVITY C e n t e r and a c t i v i t y t h a t p r e p a r e d document. �EXPLANATION OF 'ECJ~IATOF INTERFACE DOCUMENT LOG FOR APOLLO (CONTINUED) NOTES: 1. A Scheduled R e l e a s e d a t e of 9-09-99 2. S e l e c t i o n o f "Sched Re1 Dates" i s based o n t h e workload i n v o l v e d i n c o m p l e t i n g t h e document a t a t i m ~which a l l o w s f o r reasonable r e v i s i o n s p r i o r t o completion of f a b r i c a t i o n o r o p e r a t i o n a l procedures. 3. R e q u e s t s f o r c o p i e s o f I C D 1 s may b e s u b m i t t e d by t e l e p h o n e o r ,MSFC Form 4 3 3 , Request f o r Documentation, t o t h e George C . M a r s h a l l S p a c e F l i g h t C e n t e r , Documentation R e p o s i t o r y Branch (MS-D), B u i l d i n g 4494, t e l e p h o n e 876-1371 o r 876-7532, H u n t s v i l l e , Alabama 35812. The Documentation R e p o s i t o r y Branch s h a l l r e f e r r e q u e s t s w i t h a d o u b t f u l "Need-to-know" t o t h e T e c h n i c a l S t a f f Off i c e (R-S) i n d i c a t e s t h e Scheduled Released d a t e i s not determined. . �APOLLO INTERFACE CONTROL DOCUMENT LOG PANEL CODES PANEL Me~;;?!nicdl I n t e g r z t ion E l e c t r i c a l S y s tenis I n t e g r a t i o n F l i g h t M e c h a n i c s , Dynamics & C o n t r o l Flight Evaluation Crew S a f e t y F l i g h t Control Operaticns I n s t r u m e n t a t i o n & Communication Launch O p e r a t i o n s LO SUB-PANELS Electrical F i r i n g A c c e s s o r i e s & M e c h a n i c a l GSE F a c i l i t i e s & Complexes P r o p e l l a n t s & Gases INTERFACE AREA DESCRIPTION CODES CODE - DESCRIPTION CODE - DESCRIPTION L a u n c h V e h i c l e (LAW VEH) S - I , S - I B , S-IC s -1I S-IV, S-IVB Dynamic T e s t V e h i c l e (DTV) I n s t r u m e n t U n i t (IU) Subordinate Interfaces Q-Eall A d a p t e r ( S e r v i c e Module) E x t e n s i o n ( S e r v i c e Module) Flight Trajectory I n s t r u m e n t a t i o n & Communication Spacecraft L a u n c h E s c a p e S y s tern (LES) Command Module (CM) S e r v i c e Module (SM) L u n a r E x c u r s i o n Module (LEM) LEM A s c e n t S t a g e LEM L a n d i n g S t a g e F l i g h t Control RangeIGround O p e r a t i o n a l S u p p o r t S y s t e m ( R/ GOS S) H o u s t o n (MCC-H) Mission Control Center Ground S u p p o r t Equipment (GSE) Launch Complex GSE L a u n c h v e h i c l e GSE (LAW VEH GSE) S p a c e c r a f t GSE P r o p e l l a n t L o a d i n g GSE (PL GSE) F a c i l i t i e s GSE (FAC GSE) T r a n s p o r t V e h i c l e (TRANS VEH) I n s c r u m e n t a t i o n & Communication GSE (INSTR & COFM GSE) , L a u n c h Complex (LC 3 4 , 3 7 , and 39) KSC Launch Complex 34 E C Launch ~ o m p l e x e s34 a n d 37 L a u n c h Complex H a n d l i n g Equipment L a u n c h Complex T r a n s p o r t Equipment KSC L a u n c h Complex 37 KSC Launch Complex 39 - L a u n c h I n f o r m a t i o n Exchange F a c i l i t i e s (LIEF) M i s c e l l a n e o u s (MISC) �THIS I S A SUPPLEMENTAL DISTRIBUTION LIST FOR APOLLO INTERFACE CONTROL DOCUMENT LOG (1A01) FOR THE MONTHLY RUN DATED 7 / 2 9 / 6 6 MARSHALL SPACE FLIGHT CENTER . I-MO-F (R. L. C h a n d l e r ) I-I/IB-SIVB, I-I/IB-GR I-I/IB-u I -MT -MGR . R-ASTR-I (2) (2) I-v-IU I-v-SIC I-v-SII I-I/IB-SIB GENERAL ELECTRIC CORPORATION MANNED SPACECRAFT CEXTER General E l e c t r i c Corporation A p o l l o S u p p o r t Department P. 0. Box 2500 Daytona Beach, F l o r i d a 32015 A t t e n t i o n : G.D.-4/A. Lyman (MA- 2D) A 14 (3) EB5 OF PF pH ( 2 ) PR PS5 ( 2 ) PS6 (12) (Mr. Cohen) PS7 RASPO-Bethpage, L.Z. (Mr. J o h a n s e n ) Grumrnan A i r c r a f t Co.-Bethpage, L.I. (Mr. Kangas, c / o RASPO) RASPO-M.I.T. Cambridge, Mass. (Mr. Rhine) RASPO-Downey, C a l i f . , (Mr. Ridnous) ' (5) KENNEDY SPACE CENTER PPR ( P l a n s , Programs, & R e s o u r c e s ) (48) (Mr. Wagner) OFFICE MANNED SPACE FLIGHT OMSF-MA (11) (Mr. Winn) NORTH AMERICAN AVIATION, INC. M r . Marvin T o o l e y , S-ID 12214 Lakewood Blvd Downey, C a l i f o r n i a % B u i l d i n g 8 6 (692-401) TOTAT,: A l l a d d i t i o n s , d e l e t i o n s , q u e s t i o n s , a n d / o r problems c o n c e r n i n g t h i s l i s t a r e t o b e r e f e r r e d t o Nr. blndison E s t e s , R-P&VE-VSD, 876-5910. 103 (4) �DATE 2 9 JUL 66 -- --- -- -) --,= H C; I AO? APOLLO INTERFACE CONTROL 335UMtfLT 1 G r C ~ h * ' s T r iT14YE C O S T 6 3 L) S DOCUMENT NUMBER? '3R R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER A XU TO SPACECRAFT PHYS REQ SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO DA YR CODE 02-10-65 MI PREPAI INTERFACE AREAS CENTEl OR C E I NUMBERS A C T I V l 000-1 00 MSFC-F �DATE 29 J U L 66 PAGE -- --- -- SCHED ACTUAL R E L DATE R E L DATE PANEL MO D A Y R MO D A YR CODE . D S DOCUMENTNUMBERo OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER ---2 PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVTTY - B ' L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 2 0 1 - 6 6 - 0 1 7 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 7 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 5 B L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 201-66-0145 * IRN-CCBD 201-66-0145 IRN-CCBD 201-66-0175 - D 13M20217 - I U TO SPACECRAFT PHYS REQMTS ICD-CCBD 201-66-0170 IRN-CCBD 201-66-0170 IRN-CCBD - 2 0 1 - 6 6 - 0 1 7 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 2 IRN-CCBD 201-66-0170 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 2 IRN-CCBD 2 0 1 - 6 6 - 0 2 9 7 SPACECRAFT T O Q B A L L PHYS REQ IRN-CCBD 2 0 1 - 6 6 - 0 1 9 8 IRN-CCBD 201-66-0198 IRN-CCBD 2 0 1 - 6 6 - 0 1 9 8 ENVELOPE L E M / S - I V B / I U CLEARANCE PHY ICD-CCBD 2 0 1 - 6 6 - 0 1 6 4 8 SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 . EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 201-66-0114 08-17-65 IC 000-100 MSFC-ASTR �C / 1 I AOI APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATt 29 JUL 6 6 _7) PA( -- --- -- -1 c H G 1 --- D S - DOCUMENT NUMBER? OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ A L V TO SC ICD-CCBD IRN-CCBD I RN-CCBD AFRMOll I / C 201-66-0059 201-66-0059 20 1 - 6 6 - 0 2 9 8 INTERFACE SCHED ACTUAL R E L DATE R E L DATE PANEL NO DA YR Y O DA YR CODE -------- --------- ------ PREP, I N T E R F A C E AREAS CENT1 ACTI' OR C E I NUMBERS ---- % .---,. 06-14-65 IC 000-100 MS FC- I3 D E S I G N C R I T E R I A FOR SAT I B ONBOARD EDS ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 08-06-65 CS 000-10C MSFC - 02-28-66 C-S 000-100 MSFC- 03-18-65 €1 230-300 MSFC 08-12-65 €1 300-100 MSC 10-05-65 E-I 220-230 MSC-E 08-06-65 E l 220-2 5 0 MSFC- 04-09-65 El 210-220 MSFC- - EDS L I M I T S ICD-CCBD 2 0 1 - 6 6 - 0 2 2 5 E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 COMP I N T F A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 50 1 - 6 6 - 0 0 8 3 - COMP I N T E R F A C E PROGRAMMING REQUIREMENTS SC-0 1 1 / S A - 2 0 2 ICD-CCBD 2 0 1 - 6 6 - 0 0 8 2 A LV ESE TO PROPELLANT SYS AND ECS IRN-CCBD 20 1 - 6 6 - 0 1 7 9 - LV NO NO NO NO NO NO NO ESE TO LAUNCH EQUIPMENT IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD , ENTERED IRN-CCBD ENTERED 4 - SAT 18 LV E S E T O SC ESE �. A P O L L O I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 65 PAGE -- --- -- . DOCUMENT NUMBER, DR R E V 1 S I o N N O T I C E SCHED ACTUAL R E L DATE R E L DATE PANEL MO D A YR MO DA YR CODE DOC REV DOCUMENT T I T L E OR C C B D NUMBER _ --_-------------------........................................ 5 4 P K E P A R IPIG I N T E R F A C E AREAS CENTE' OR C E I NUMBERS A C T I V . . . r -------- -------- ------ --------------- --------- I ICD-CCBD 201-65-0042 IRN-CCBD 201-66-0180 IRN-CCBD 201-66-0180 I RN-CCBD 201-66-0308 NO IRN-CCBD E N T E R E D I R N - C C 8 0 20 1-66-033 1 .IRN-CCBD 201-66-0331 4 40M37528 B I N S T U N I T T O S P A C E C R A F T E L E C T REQ 1 40M37532 A D E S O F SAT S A - 2 0 2 + APOLLO S C - O l l ICD-CCBD 201-66-0220 NO IRN-CCBD E N T E R E D R 2 EDS 03-11-66 E-I MSFC-ASTR 05-09-66 C-S F1SFC-ASTR A E D S CHECKOUT S C H E M A T I C S ICD-CCBD 20 1-65-0046 NO IRN-CCBD E N T E R E D \ 50M12614 - 07-1 5-66 IC 280-290 MSFC-ASTR 07-1 5-66 IC 280-290 MSFC-ASTR 07-15-66 IC 280-290 MSFC- ' IC SEE-DWG MSFC-ASTR S / C ESE/GSE 07-23-65 LOFC 230-340 A L C 3 4 DATA T R A N S M I S S I O N S Y S ( W I D E BAND) NO IRN-CCBD E N T E R E D - NO IRN-CCBD E N T E R E D .09-24-65 LOFC 230-340 A L C 3 4 F A C I L I T Y INST. 02-02-65 LO-FC DEF SAT I B S R S C T E S T ENCOD/LC-34+LC-37 - DEF - DEF - DEF S R S C DECODER/LC-34 + LC-37 INTF S A T I B S R S C IND .PANEL/LC-34+LC-37 S A T I B S R S C CODE PLUG/DECODER B L C 3 4 S I T E PLAN-FACILITY-TO CABLING SYSTEM INTF 07-15-66 KSC R' * �APOLLO I N T E R F A C E CONTROL DDCUMEiUT L C t \ H 0 f. - c7 ) PAG -- --- - DATE 2 9 JUL 66 I 1 IA01 --- DOCUMENT NUMBEKp 3 2 REVISION NOTICE DOC REV DOCUMENT TITLE OR C C B D NUMBER -------------------- --- -----------_--_-------------------------- - L C 3 4 AC E L E C T POWER SYSTEM A L C 3 4 SAT I B S / C 65 I C D 5 0 0 7 , - LC-34 TRANP. 0 3 - 1 5-65 LOFC 230-340 KSC-F 12-02-65 LOFC 230-340 KSC-El 02-28-66 LOEL 230-340 KSC 08-1 1-65 LOEL 210-340 KSC-L' 09-14-65 LOPG 100-230 KSC-E ESE/GSE 06-03-65 LOFC 230-340 KSC-F ESE/GSE 07-23-65 LOFC 230-340. KSC-E GSE P I P C R I T + I N T F LOC S I C FLD SYS L C 3 4 S S NO fRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED B L C 3 4 S E R V I C E STRUCTURE -TO NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED, S/C --------_-- --- ----KSC-F A L C 3 4 HAZARD PROOF MONXTORIMG FOR S / C NO IRN-CCBD ENTERED E 651CD5200 R 1 R 2 R 3 R 5 R 6 -a_--- 230-340 ROUTES CONTROL CENTER-S/C ENTERED ENTERED ENTERED ENTERED ENTERED -------*-- LOFC HAZARD PROOFING S / C ESE/GSE B L C 3 4 LAUNCH NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD -------- PREPA I N T E R F A C E AREAL CENTE OR C E I NUMBERS ACTIV 11-25-64 D LC 3 4 CSM E S E T O F A C C A B L I N G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - SCHED 4CTUAL R E L DATE R E L DATE P A N E L MO DA YR MO DA Y R CODE �' APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 PAGE -- --- -- Ll S DOCUMENT NUMBER, DR R E V I S I O N NOTICE DOC REV SCHED ACTUAL DATE R E L DATE PANEL MO D A YR MO D A YR CODE REL CCBD DOCUMENT T I T L E OR NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NUMBER f --- PREPhRING INTERFACE A R E A S CE?d' OR C E I NUM8ERS ACflVITY - ENTERED ENTERED ENTERED A L C 3 4 PAD AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 07-23-65 ESE/GSE LOFC i C L C 3 4 PAD AREA MECH GSE 09-16-64 LOFC 230-340 KSC-F - FUNCT I N T E R F A C E REQ ECS L C 3 4 S/C-GSE 01-27-65 LOPG 100-340 KSC-K-DT - FUNC I N T F REQMTS GHE L C 3 4 S / C GSE 09-1 5-65 LOPG 100-230 KSC-euv FUNC I N T F REQMTS GN2 L C 3 4 S / C NO IRN-CCBD ENTERED GSE 09-1 5-65 LOPG ' 100-230 KSC-EDV FUNC I N T F REQMTS GOX LC34 S / C GSE - - - C R I T + I N T F LOC S / C ENTERED ENTERED ENTERED L C 3 4 SERV STRUCTURE-GSE-LAUNCH - -. I A L C - 3 4 I N T E R F A C E S / C GSE T O UMB THR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD I 09-15-65 LOPG 100-230 KSC-EDV 04-05-66 LOFC 230-340 KSC-FCV 06-1 8 - 6 5 LO-FC 200-340 XSC-P9VE F L D SYS VEHICLE ' �APOLLO I N T E R F A C E COPIT R O L OOCUMENT LL' PAC; -- --- -- C H u G S --. 3 IA01 DATE 2 9 J U L 66 1 j - DOCUMENT NUMBER* 3K R E V I S I O N N O T I C E .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ---------------------------------------- SCHED ACTU4L R E L DATE R E L d A T E PANEL MO DA YR NO DA YR CODE PREPAl I N T E R F A C E A k E A S CElVTEl OR C E I NUMBERS ACTIV. ------PC -------.---...?--C-. --I-)-.=--- ------- ------ ICD-CCBD 2 0 1 - 6 6 - 1 4 0 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED I A LC34 PAD AREA/GSE-L/V ICD-CCBD 2 0 1 - 6 6 - 1 3 8 - 09-29-65 LO-FC 220-340 KSC-EL: 01-1 0 - 6 6 LO-FC 000-340 KSC-EC 10-06-65 LO-EL 220-340 MSFC-0 05-28-65 LO-EL 220-340 MS FC-b 08-12-65 LOEL 220-340 MSFC-E 02-1 8-66 LO-EL 220-200 MSFC-8 MSFC COUNT CLOCK TO KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 06-09-65 LO-EL 200-240 MSFC-6 LV ESE TO KSC D A T A MEASUREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 4 6 12-1 5-65 L C 3 4 PHY I N T F S - I B STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 1 3 9 A t V ESE TO F A C I L I T Y C A B L I N G L C - 3 4 ICD-CCBD 2 0 1 - 6 6 - 0 3 4 4 NO IRN-CCBD ENTERED - - L V ESE T O RANGE SEQUENCING L C - 3 4 ICD-CCBD 2 0 1 - 6 5 - 0 0 3 6 LV NO NO NO E S E TO F A C I L I T Y AC POWER L C - 3 4 IRN-CCBD ENTERED IRN-CCSD ENTERED IRN-CCBD ENTERED A L V ESE TO I N S T R S Y S ICD-CCBD 2 0 1 - 6 5 - 0 0 3 8 A 65ICD5605 - + RECORDERS LO-EL 220-340 MSFC-6 �IAOl APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE -- --- -- DATE 29 J U L 66 DOCUMENT NUMBERI R R E V I S I O N NOTICE R (J j1 8 --- i3 '.- DOC REV - SCHED ACTUAL REL DATE REL DATE PANEL H O DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD 1 - 2 0 1-66-0146 L V ESE TO WATER DELUGE SYSTEM ICD-CCBD 2 0 1 - 6 5 - 0 0 4 0 IRN-CCBD 2 0 1 - 6 5 - 0 0 4 0 PHY I C D S - I V B A PHY I C D ICD-CCBD IRN-CCBD IRM-CCBD IRN-CCBD PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y -------- -------- ----- ----------- B SAT* T O P I P C R I T + I N T F LOC APS PPOP . ICD-CCBO 2 0 1 - 6 6 - 1 4 2 51CD5741 1 APS PORTABLE VALVE BOX APS HODULES ON L A U VEH/SAT 201-66-143 201-66-0143 201-66-0239 201-66-0234 IB A PHY I C D PNEUMATIC CONSOLE DSV-40-433 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 ---------- 3' 0, 05-28-65 LO-EL 220-340 HSFC-ASTR 02-1 1-66 LO-PG 220-347 MSFC-EDV 07-26-65 LOPG 220-340 KSC-P+VE 11-10 - 6 5 LO-FA 040-347 HSFC-EDV ~3 '-) ./ A P I P I N G C R I T E R I A S - I V B APS PNEU U N I T S / I B ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 . IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 A PHY I C D PNEUMAT IC. CONSOLE DSV-4B-432/ ICD-CCBD 2 0 1 - 6 6 - 0 2 8 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 8 . IB 11-1 0 - 6 5 LO-FA 040~347 MSFC-EDV 0. \- 10-25-65 03-02-66 LO-FA LO-FA 220-347 220-347 KSC-K-DT KSC-K-DT 0 a, I -0. 1 �APOLLO I N T E R F A C E CONTROL DOCUMENT LC:; D A T t 29 JUL 66 -- --- -SCHED ACTUAL R E L DATE REL DATE PANEL MO DA YR MO DA Y R CODE C E ' * D S DOCUMENT NUMBER9 OK R E V I S I O N N O T I C E - - -------------------- DOC REV -Y- DOCUMENT T I T L E OR CCBD NUMBER A PHY I C D PNEUMATIC CONSOLE D S V - 4 8 - 4 3 6 / I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 * J 65ICD5883 * R J 651C05888 '> R 7 9 -\ J 651CD5889 R 1 ...-------------------- ---LO-FA 220-347 KSC- 04-12-65 LO-FA 220-347 KSC- A P I P I N G C R I T E R I A S I V B STAGE PNEU SUP SYS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 02-04-66 LOFA 040-347 MSFC A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 COFA 040-347 PSFC A PHY I C D FWD UMB S H I N G ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 0 1 - 2 1-66 LO-FA 040-347 MSFC A PHY I C D I U UMB SWING ARM NO 3 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5-66 LOFA 090-34'1 MSFC 08-02-65 LOFA 010-347 KSC- 08-02-65 LO-FA 010-347 KSC- - - 1 2 3 5 d -*---.---- 03-02-66 1 i R R R * -------- , 3 - PRE I N T E R F A C E AREAS CEN OR C E I NUMBERS ACT - PHY I C D HEAT EXCHANGER O S V - 4 8 - 4 3 8 / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 7 P H Y I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED PHY I C D UMB CONN S - I B / I B NO IRN-CCBD ENTERFD (SH C M A S T I I ) SH M A S T I V . , ��< * I il i I i i -> ?' APOLLO I N T E R F A C E CONTROL DOCUMENT 101; -; D A T E 2 9 J U L 66 -- --- -- , f / fi Ci H D s DOCUMENTNUMBER? j i R t v I s I o N NOTICE DOC Riv SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER ........................................ P INTERFACE AREPS C OR C E I NUMBERS A P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 12-30-65 LO-FA 220-347 M PHY I C D VACUM M O N I T O R I N G CONSOLE SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 4 1 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 5 01-10-66 LO-FA 040-347 K. 18 PHY I C D I U C O O L I N G U N I T L C 3 4 ALTERNATE NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 PHY I N T F CONT DUG IU FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 6 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 LC/34/37/39 S/C A-C. T I M I N G + COUNTDOWN O I S T POWER RECe + CONN LC 3 4 / 3 7 / 3 9 SM SWG ARH UMB D I S C A 1 4 0 1 9 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED L C 3 4 / 3 7 / 3 9 CHD MOD ACCESS ARH C A B L I N G NO IRN-CCBD ENTERED VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED C / M ACCESS A R M ADPT H O O O TO S / C I N T F REQ L C 3 4 / 3 7 SH ARM E L E CABLE + F L T R B O X . I N S T 12-16-t)S LO-FA 290-347 K.T �. APOLLO INTERFACE CONTROL DOCUMkNT L O G 2'1 J U L 6 6 UATI D _ 5 -- AS ...- DOCUIlENTNUMBERc OR R E V I S I O N NOTICE __-PP---P--s..D--O- R 202 CON?, PAGE -..,.-.-- ---- DOC REV - DOCUMENT T I T L E OR CCBD NUMBER ---.a=>--- --U-P-IPI-LI--------------~==----~-.-=-~~~-=---=~- ---P ? NO IRN-CCBD - LC34/37 - S-IB - - PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACT? TY - -------------- ----- ----- --.------ --..-->- 07-01-65 LO-FC 07-01-65 LOVC 05-07-65 LO-PG 220-347 KSC-DP 02-23-66 LOPG 000-220 KSC-EDY ENTERED L/V+S/C MISALIGN, FOR SAT I B VEH LV PROTUBERANCES L C 3 4 / 3 7 FUNCT I / F F L D RQMTS-ECS-SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 7 IB-L/V GSE A FUNC I N T F F L U I D REQMTS GN2 SYS SAT I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 - SCHED ACTUAL REL DATE R E L . D A T E PANEL MO DA YR MO DA YR CODE 1; --- 200-347 501-66-0039 MSFC-P+VE MSFC J' t FUNC I N T F F L U I D REQMTS GN2 SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 I RN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 05-25-65 LO-PG 000-220 KSC-K-DT FUNC I N T F F L U I D REQMTS L H 2 SYS SAT I 8 ICD-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 05-24-65 LO-PG 000-220 KSC-R-DT �APOLLO I N T E R F A C E CONTROL DUCUMENT L u UATf PAGE 29 JUL 6 6 -- --- -- c H G il DOCUMENT NUMBERP 3 R R E V I S I O N NOTICE DOC REV A 65ICD8605 . R R 1 2 I , - ' - DOCUHENT T I T L E OR CCBD NUMBER - PREPAR I N T E R F A C E A R E A S CENTER OR C E I NUMBERS ACTIVI IB 05-24-65 LO-PG 000-250 KSC-K- FUNC l N T F F L U I D REQMTS LOX SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 05-25-65 LO-PG 000-250 KSC-K- FUNC I N T F F L U I D REQMTS RP-1 ICD-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 05-25-65 LO-PG 000-250 KSC-K- 12-10-65 LO-FA 110-300 KSC-ED' 12-10-65 LO-FA 220-347 MSFC-El 02-11-66 LO-EL 220-24'0 % 1 09-27-65 FM 000-1 00 MSFC-AI FUNC I N T F F L U I D REQMTS L H 2 SYS SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 7 3 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 3 SYS SAT I 8 PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD - SCHEP ACTUAL R E L DATE R E 1 D A T E PANEL t4O DA Y R MO DA YR CODE COVER-.- 501-66-0164 PHY I C D HAZARDOUS GAS ANALYZER SATURN I B 1CD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 LOW BAY ESE T O I N S T R U SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 + REC FC �UArt PAGE 39 J U L 66 -- ---- -- DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DD'C REV _------------------- --13M06399 A DOCUMENT T I T L E OR C C B D NUMBER SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO D A YR CODE --17-1 PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY - ;-I '.-' ' ----P--------Qu--Q-------=~-,---.~-----~--- CRYOGENIC STOR S Y S / L V ICD-CCBD 2 0 1 - 6 6 - 0 0 2 4 I R N - C C B D 201-66-0176 PROCEDURAL REQ CRYOGENIC STOR S Y S / L V I C D - C C B D 201-66-0174 F U N C T I O N A L REQ CRYOGENIC PHYSICAL ICD-CCBD IRN-CCBD S T O R SYSILV 20 1-65-0026 2 0 1-66-0026 REQ /' MSFC B SATURN/APOLLO FREQ P L A N I C D - C C B D 50 1 - 6 6 - 0 2 5 6 - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 't \ . . I '7 MSFC-ASTR ',' 7 B D E S I G N C R I T E K I A FOR S A T I B ONBOARD EDS ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 16331-634107350 16331-63A107393 - E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 - (... COMP I N T F A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - MSFC L V ESE/PROPELLANT SYSTEMS I C D - C C B D 201-65-0047 I R N - C C B D 20 1 - 6 6 - 0 0 9 4 L V ESE/LAUNCH EQUIPMENT JCD-CCBD 201-65-0048 ([I) COMP I N T E R F A C E MSC MS F C - A S T R MSFC-ASTR <j �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G AS DATE 2 9 J U L 66 -- --- -- / 203 ----- c H G ,,,: S DOCUMENT NUMBERc OR R E V I S I O N N O T I C E DOC REV --- ,, , , , , , , , , , , , , , , , - - - SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVX -------- -------- ------ --------------- ----,--,-,,,,,,------------------------ IRN-CCBO - PAGE CONTO 0----- 20 1 - 6 6 - 0 0 9 5 DEF OF SATURN S A - 2 0 3 ICD-CCBD 20 1 - 6 6 - 0 0 5 4 4 MSC EXP ELEC I N T SAT APOLLO EDS C/O SCHEMATICS ICD-CCBD 2 0 1 - 6 6 - 0 0 7 s I C D D E S C R I P T I O N OF SATURN S A - 2 0 3 ICD-CCBD 2 0 1 - 6 6 - 0 0 6 2 EDS 10-26-65 E-I 000-100 MSFC-A 03-24-66 €1 000-220 MSFC-A 10-15-65 CS - DEF SAT I B I U CMD S Y S G S E / L C - ~ ~ + L C - ~ ~ 07-1 5 - 6 6 IC 280-290 MSFC-A - DEF SAT I B SRSC T E S T ENCOD/LC-34+LC-37 07-15-66 IC 280-290 MSFC-A 07-15-66 IC 280-290 MSFC-A 07-1 5 - 6 6 IC 280-290 MSFC-A 07-15-66 IC SEE-DUG MSFC-A - - DEF SRSC DECODER/LC-34 + LC-37 INTF D E F S A T I B SRSC I N D P A N E L / L C - 3 4 + L C - 3 7 DEF SAT I B SRSC CODE PLUG/DECODER INTF FUNC I N T F REQMTS GHE L C 3 4 S / C GSE 09-15-65 LOPG 100-230 KSC-ED FUNC I.NTF REQMTS GN2 L C 3 4 S / C NO IRN-CCBD ENTERED GSE 09-1 5 - 6 5 LOPG 100-230 KSC-ED FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-1 5 - 6 5 LOPG 100-230 XSC-ED 04-05-66 LOFC 230-340 KSC-ED A L C - 3 4 I N T E R F A C E S / C GSE T O UMB TWR NO IRN-CCBD ENTERED NO IRN-CCDD ENTERED' NO IRN-CCBD ENTERED �A P U L L O I N T E R F A C E CONTROL DOCUMENT LOG PAGE DOCUMENT NUMBER* SCHED ACTUAL' R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE DOC O R R E V I S I O N N O T I C E REV -----------.-.--___----- DOCUMENT T I T L E OR CCBD NUMBER -------- --_------YI-----P----------------------- * A PHY I C D APS MODULES ON L A U V E H / S A T ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A P I P I N G CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCUD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCSD 2 0 1 - 6 6 - 0 2 8 1 LO-PG ----em---- 220-347 , (> , - MSFC-EDV f-: 11-10-65 IB LO-FA 040-347 MSFC-EDV 11-10-65 LO-FA 040-347 MSFC-EDV 4 ?..--) -.. 10-25-65 A PHY I C D PNEUMATIC CONSOLE D S V - 4 8 - 4 3 3 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 03-02-66 LO-FA 220-347 KSC-K-DT 03-02-66 LO-FA 220-347 KSC-K-DT A PHY ICD PNEUMAT I C CONSOLE D S V - 4 8 - 4 3 6 / ICD-CCBD 2 0 1 - 6 6 - 0 1 3 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 *\ L,) APS PNEU U N I T S / I B PHY I C D HEAT EXCHANGER D S V - 4 0 - 4 3 8 / I B -1CD-CCBD 2 0 1 - 6 6 - 0 2 8 7 ISN-CCBD 2 0 1 - 6 6 - 0 2 8 7 .- '_j INTERFACE AREAS C E N T E R OR C E I NUMBERS ACTIVIT'L A PHY I C D PNEUMATIC CONSOLE D S V - 4 8 - 4 3 2 / I B ICD-CCBD 201-66-0288 IRN-CCSD 2 0 1 - 6 6 - 0 2 8 8 - l 6 k L , PREPARING -I..,.-*-.- 02-1 1-66 B SAT 1 B P I P C R I T I N T F LOC APS PPOP ICD-CCBD 2 0 1-66-142 -) --- I8 LO-FA 220-347 KSC-K-DT (. +' % /> - 04-12-65 LO-FA 220-347 KSC-K-DT -1 (3 . �._' APOLLO I N T E R F A C E CONTROL DOCUMENT L O G ? DATE 29 JUL 6 6 ' J . .. -- --- -- AS 203 ----- CON?, 7c a-i H - U DOCUMENT NUMBER* DOC S OR R E V I S I O N NOTICE REV DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR HO D A YR CODE PREF I N T E R F A C E AREAS C E N l OR C E I NUMBERS ACT1 -------- -------- ------ --------------- ---- A P I P I N G C R I T E R I A S I V B STAGE PNEU SUP SYS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED I - 3 651CD5885 R 3 * I* 2 J 65ICD5886 R R 1 2 A PHY I C D AFT UMB SWING A R M NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 MSFC A PHY I C D FWD UM8 S W I N G ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-2 1-66 LO-FA 040-347 M S FC 08-02-65 LOFA 010-347 KSC- 08-02-65 LO-FA 08-02-65 LO-FA A - - - PHY I C D I U UMB S W I N G ARM NO 3 NO IRN-CCBG ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ' ENTERED ENTERED ENTERED ENTERED (SH C MAST111 SH M A S T I V PHY I C D OBAT T A I L L O X UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - Q 2 8 4 , 010-347 KSC- �A P U L L O I N T E R F A C E CONTROL DOCUMENT LOG AS DOCUMENT NUMBER, OR R E V I S I O N N O T I C E 651CD5891 R DOC REV - 1 - - 203 CONTo SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR M O D A YR CODE DOCUMENT T I T L E OR CCBD NUMBER P H Y S I C A L I C D BOAT T A I L F U E L UMB S--IHI ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PAGE -- --------.16 FWD (SW ARM f l l -->-- 08-02-65 LO-FA PREPARIw'S I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y -----------em- 010-347 ---------- <-)-. KSC-P+VE \: \-.. 08-02-65 LO-FA 010-347 KSC-P+VE -. 1~;) . -- ;J . ,- .-/ : 08-02-65 LO-FA A A PHYS I C D I N S T R U N I T PNEU CONSOLE/ I 8 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 03-02-66 LO-FA 12-30-65 LO-FA 010-347 KSC-P+VE 040-347 MSFC-EDV A PHY I C D S - I V B / I U C O O L I N G U N I T / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - c) .('.- PHY I C D BOAT T A I L COND UMBLS S - 1 6 / 1 0 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 - 18':;) P I P I N G C R I T E R I A INSTRUMENT U N I T LC34-3; ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 PHY I C D VACUM M O N I T O R I N G CONSOLE SAT I 0 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 1 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 5 8 �.j > . r - -* -- A P O L L O I N T E R F A C E CONTROL DOCUMENT LOG * PA! DATE 2 9 J U L 6 6 ‘) -- --- -- ,-JC H U DOCUMENTNUMBERp OR R E V I S I O N N O T I C E f S 3--- .................... DOC REV DOCUMENT T I T L E OR C C B D NUMBER --- ......................................... A 7Q J ~r 3 J 651CD5899 R 1 A 65ICD6005 A 65ICD6466 -------- PREP I N T E R F A C E AREAS CENT OR C E I NUMBERS ACTI' ------ --------------- ---- -I------ PHY I C D I U C O O L I N G U N I T L C 3 4 ALTERNATE NO I R N - C C B D E N T E R E D IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 A PHY I N T F CONT DWG I U FLOW CONT V A L V E BOX I C D - C C B D 201-66-0104 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-16-65 LO-FA 290-347 KSC-I - 03-1 5-65 LOFC 230-370 KSC-F A L C 3 7 S A T I B S I C T R A N S P O R T ROUTE 03-1 5-65 LOFC 230-370 KSC-f - 02-08-66 LOFC 230-370 KSC A F A C I L I T Y C A B L I N G L C 3 7 F O R L E M +ESM 05-20-66 LOEL 230-370 KSC-I - 02-16-66 LO-EL 230-340 MS FC- LC37-S/C S E R V I C E STRUCTURE ESE/GSE NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D 08-17-65 LOFC 230-370 KSC-I FUNCT I N T E R F A C E REQS ECS L C 3 7 8 S/C-GSE 03-19-65 LOPG 100-37G KSC-l LOPG 100-370 09-1 6 - 6 5 LOFA 230-370 K SC- 12-08-65 LO-FC 220-370 K SC- - 9 SCHEO ACTUAL R E L DATE REL DATE PANEL MO D A YR MO D A YR CODE - L C 3 7 OPNL T V S Y S LC 3 7 H A Z A R D P R O O F I N G S / C NO I R N - C C 8 D E N T E R E a SC E S E T O D C POWER S U P L D I S T I C D - C C B D 201-66-0077 + F U N C T X N T F REQMTS 0 2 L C 3 7 B S / C AC I N P U T GSE A L C 3 7 B UT P I P C R I T + I N T F L O C S / C F L D SYS 08-01-65 _ KSC-8 �. APULLO I N T E R F A C E CONTROL DOCUMENT LOG OATt 23 JUL 6 6 ---- -- DOCUMENT NUMBER* OR R E V I S l O N N O T I C E --20") PAGE DOC REV _------------------- --- DOCUMENT T I T L E OR CCBO NUMBER --..----------.-----.~Q~--I----------------- ICD-CCBD SCHED ACTUAL REL D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE --.=1----- -em--.--- L PREPARING I ? L.1 I N T E R F A C E AREAS CENTER , OR C E I NUMBERS A C T I V I - - -.----.I-.--- LD-------------- 1-'(L, 201-66-0113 ,--\ - 4 2 ' L C 3 7 PAD AREA E S E I G S E - L / V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 02-10-66 LO-FC 220-370 KSC L C 3 7 PHY I N T F S - I B STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 0 1 0 1 01-1 0 - 6 6 LO-FC 000-370 KSC-EDV 01-25-66 LOEL 220-210 MSFC-ASTR A F A C I L I T Y CABLES L C - 3 7 B IRN-CCBD 2 0 1 - 6 6 - 0 2 0 5 - FOR LV ESE L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 2 1 02-1 1-66 LO-EL A L V E S E I I N S T R U M E N T A T I O N SYS + RECORDERS 03-1 4-66 LOEL - 08-09-65 LO-EL LO-EL 220-200 MSFC-ASTR - - f../ -.! \ MSFC-ASTR MS FC-ASTR -- ICD-CCBD - LC/34/37/39 T I M I N G + COUNTDOWN D I S T L C 3 4 / 3 7 SM ARM E L E C A B L E + F L T R BOX I N S T (L! c-; -, L V ESE T O KSC DATA MEASUREMENTS L V ESE TO WATER DELUGE SYS ICD-CCBD 2 0 1 - 6 5 - 0 0 5 2 \ ,._i 08-17-65 MSFC COUNTCLOCK TO KSC T I M I N G 201-65-0051 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 1 ,( SAT I E L V E S E T O RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 6 - +r -- MSFC-ASTR 07-13-66 LO-EL MSFC-ASTR b 09-22-64 (3 0 LO-FC KSC-DE t -- �- APOLLO I N T E R F A C E CONTROL DUCUMENT LOG - D A T E 2 9 J U L 66 -- --- -- -> 1 SCHEC ACTUAL R E L DATE R E L DATE P A N E L N O D A YR MO DA YR CODE !, C ti i; -, '1 )* D ' DOCUMENT N U M B E R , 38 R E V I S I O N NOTICE R DOC REV NO IRN-CCBD 1 J 65ICD8401 DOCUMENT T I T L E OR CCBD NUMBER 1 - -------- -------- ------ --------------- ,; A 65ICD8603 - -----. ENTERED t C 3 4 / 3 7 L/V+S/C M I S A L I G N o FOR SAT I B VEH S - I B L V PROTUBERANCES L C 3 4 / 3 7 FUNCT I / F F L D RQMTS-ECS-SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 7 IB-L/V GSE A - F U N C I N T F F L U I D REQMTS GN2 SYS S A T I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED " NO iRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1-66-0207 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 - PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV FUNC I N T F F L U I D REQMTS GN2 SYS S A T I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 5 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 I RN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 FUNC I N T F F L U I D REQMTS L H 2 SYS S A T I B ICD-CCBD 2 0 1 - 6 6 - 0 1 2 8 , 200-347 MSFC-I 07-01-65 LO-FC 07-01-65 LOVC 05-07-65 LO-PG 220-347 KSC-Df 02-23-66 LOPG 000-220 KSC-EI 05-25-65 LO-PG 000-220 KSC-K- 05-24-65 LO-PG 000-220 KSC-K- 501-66-0039 MSFC �4 ~ n l . l nI N IF R F ACE C O N T R O L DoC~IMEFIT L O G 11:~ I . LJ '{\ION NQrlCE I , : J T qUMfit.Hp .-.... GUb RkJ - a .* t 1, . . 1 : '*c4; , ............................. - . 0 . .... ..- CUNT P;I!I:~;~:~ F U N C l N r F F L U I U K t O H T S LH2 S Y S S A T 18 ,I. SCHED ;,c 7 1I #,I. K E L DATE I ~ " L I d f i+t - I J r r I L M O D A Y R M I J D,] { Y C ~ I I: ' ........ 05-24-65 LO-PG L~--.IJ>-'J:J~; ;,3-,Lda . .#,.I - .. ;. , , ,'s ..~t,;,.-l.*, ' .I i.ti')!>-,? 5 !J MSC-K-UT !-, ,\>. L?-in-h5 65ICD8702 R R - PYY - P H Y ICD HAZARDOUS GAS A N A L Y Z E R S A T U R N I B TCD CALIF'< C / O CONSOLE SAT I 8 LO-FA 02-04-66 LOFA 12-10-65 LO-FA 02-11-66 LO-EL ICD-CCBD 201-66-0102 NO IRN-CCSD ENTERED IRN-CCBD 201-66-0279 1 2 - LOH B A Y ESE TO INSTRU ICD-CCBD 501-6%-0171' SYS + REC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl \ 1 !c -- --- -- H U --. S G .i--- PAGE DATE 2 9 JUL 66 1 DOCUMENT NUMBER^ OR R E V I S I O N NOTICE .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO D A Y R MO D A YR CODE -------- -------- ------ PREPAF I N T E R F A C E AREAS CENTEF OR CEI NUMBERS ~ C T I V --------------I ------ PROCEDURAL REQ 12-14-65 MI 000-100 MSFC-P B L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 2 0 1 - 6 6 - 0 1 4 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 7 5 12-14-65 MI 000-100 MSFC-F 12-07-64 MI 000-100 MSFC-F 01-08-65 HI 000-140 MSFC-I 05-10-66 IC 000-100 MSFC EM1 COMPATIBILITY DESIGN CRITERIA ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 08-17-65 IC 000-100 -MSFC-I L V T O S C 0 1 2 I N S T R + COMM I N T E R F A C E 08-02-65 IC 000-100 MSFC-, 8 L A U VEH/SPACECRAFT ICD-CCBD IRN-CCBD IRN-CCBD - - - 201-66-0175 201-66-0175 2 0 1-66-0185 I U TO SPACECRAFT PHYS REQMTS ICD-CCBD 2 0 1 - 6 6 - 0 1 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 9 IRN-CCBD 201-66-0169 SPACECRAFT TO 9 - B A L L ICD-CCBD 2 0 1 - 6 6 - 0 1 6 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 5 ENVELOPE L E M / S - I V B / I U ICD-CCBD 201-66-0162 PHYS REQ CLEARANCE PHY B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 29 JUL 66 AS -- --- -- O S UOCUMfNTNUMBERv OR R E V I S I O N NOTlCE 204 IA01 CONT. PAGE ---em DOC REV OOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD IRN-CCBD IRN-CCBD - MSFC i EDS L I M I T S E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 07-1 5-66 COMP I N T F COMP I N T E R F A C E PROGRAMMING REQUIREMENTS S C - ~1 2 / ~ ~ - 2 0 4 ICD-CCBD 2 0 1 - 6 6 - 0 0 8 3 A L V ESE TO PROPELLANT S Y S AND ECS IRN-CCBD 2 0 1 - 6 6 - 0 1 7 9 - - ,- -------- -------- ------ --------------- ----- --- I B ONBOARD EDS A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTIVITY 201-66-0058 201-66-0058 201-66-0058 201-66-0058 8 D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 - SCHED ACTUAL R E L DATE R E L DATE PANEL 140 DA Y R MO D A YR CODE --24,--- LV NO NO NO NO NO NO NO ESE TO LAUNCH EQUIPMENT IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED L V E S E / P R O P E L L A N T SYSTEMS 03-18-65 C-S MSFC-ASTR €1 MSFC MSC - '-. . HSC 1- MSFC-ASTR :, .'. \. MSFC- WSFC-ASTR ,' '. - '. �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G - D A T E 2 9 JUL 66 -- --- -- -) -; AS .- 204 ----- C T' H D S DOCUMENT NUMBER9 OR R E V I S I O N NOTICE PAC CONT. SCHED ACTLJL R E L DATE R E L P A T E PANEL MO DA YR MO D A YR CODE DOC REV G DOCUMENT T I T L E OR CCBD NUMBER - -- -------------------- --- ........................................ PREP) I N T E R F A C E AREP.5 CENT€ OR C E I NUMBERS ACTIi d ICD-CCBD 201-65-0047 MS FC- L V E S E / L A U N C H EQUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 SAT I B LV E S E T O APOLLO S / C ICD-CCBD 2 0 1 - 6 5 - 0 0 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 6 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 6 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 2 DEF S A - 2 0 4 AND S C - 0 1 2 MS FC- ESE 01-07-66 ELEC I N T F C EI 000-100 MSFC- EDS CHECKOUT SCHEMATICS 06-30-66 EI 000-220 HSFC - D E F SAT I B I U CMD SYS G S E / L C - 3 4 + L C - 3 7 07-1 5 - 6 6 IC 280-290 MSFC- - DEF SAT I B SRSC T E S T ENCOD/LC-34+LC-37 07-1 5 - 6 6 IC 280-290 MS FC- 07-15-66 IC 280-290 MS FC- 07-1 5-66 IC 280-290 MSFC- 07-1 5-66 IC SEE-DWG XSFCKSC-f - DEF SRSC DECODER/LC-34 + LC-37 INTF DEF S A T I B SRSC I N D P A N E L / L C - 3 4 + L C - 3 7 DEF SAT I B SRSC CODE PLUG/DECODER INTF S I C ESE/GSE 07-23-65 LOFC 230-340 A L C 3 4 DATA T R A N S M I S S I O N SYS ( W I D E BAND) NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 09-24-65 LOFC 230-340 A L C 3 4 F A C I L I T Y INST, 02-02-65 LO-FC B ~ ~ 3 SITE 4 ' PLAN-FACILITY-TO C A B L I N G SYSTEM - KSC-f KSC �APOLLO INTERFACE CONTROL DOCUMENT LOG 26.3 PAGE DATE 2 9 J U L 6 6 -- --- -- --- b DOCUMENT NUMBER* OR R E V I S I O N NOTICE --I-----_-_----.,----- 65 ICD5005 DOC REV --- 65 I C D 5 0 0 6 65 ICD5007 DOCUMENT T I T L E OR CCBD NUMBER - PREPARING ;.-"! . , INTERFACE AREAS CENTER . OR C E I NUMBERS A C T I V I T Y . -----------------I-------------------*-.-- L C 3 4 AC ELECT POWER SYSTEM 11-25-64 LOFC 230-340 KSC-F 03-1 5-65 LOFC 230-340 KSC-F 12-02-65 LOFC 230-340 KSC-EDV-2 ' i l A L C 3 4 SAT I B S/C ' SCHED ACTUAL. REL DATE REL DATE PANEL MO DA YR M O DA YR CODE LC-34 TRANP. ROUTES HAZARD PROOFING S / C ESE/GSE i', ._.I D LC 3 4 CSH E S E TO FAC C A B L I N G NO IRN-CCBD ENTERED 02-28-66 LOEL 230-340 KSC '-I A L C 3 4 HAZARD PROOF MONITORING FOR S/C NO IRN-CCBD ENTERED - P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED B L C 3 4 LAUNCH NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD GSE F L D S Y S L C 3 4 SS LOPG 100-230 KSC-EDV {--, ,-,) CONTROL CENTER-S/C ENTERED ENTERED ENTERED ENTERED ENTERED B L C 3 4 S E R V I C E STRUCTURE -TO NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO, IRN-CCBD ENTERED NO IRN-CCBD ENTERED 09-14-65 S/C ESEIGSE ESE/GSE 06-03-65 LOFC 230-340 KSC-F 07-23-65 LOFC 230-340 KSC-EDVi - , .. ! I . \ .i -,:.- j ., �APOLLO I N T E R F A C E CONTROL DbCUMENT LO{, .DATE 2 9 J U L 6 6 -- --- -- C H U DOCUMENT NUMBER9 OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -S ----------_-_-_------- ........................................ 9 R 14 NO IRN-CCBD ACT3AL SCHED R E L DATE R E L DATE P A N E L HO DA YR MO DA Y R CODE PRE I N T E R F A C E AREA5 C E N OR C E I NUMBERS ACT -------- -------- ------ -------------- --- ENTERED A L C 3 4 PAD AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED ESE/GSE 07-23-65 LOFC 230-340 KSC- C L C 3 4 PAD AREA MECH GSE 09-16-64 LOFC 230-340 KSC- - FUNCT I N T E R F A C E R E 0 ECS L C 3 4 S/C-GSE 01-27-65 LOPG 100-340 K S 6- FUNC I N T F REQMTS GHE L C 3 4 S / C GSE 09-15-65 LOPG 100-230 KSC- FUNC I N T F REQMTS GN2 L C 3 4 S I C ND IRN-CCBD ENTERED GSE 09-15-65 LOPG 100-230 K S C- FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-1 5-65 LOPG 100-230 KSC* 04-05-66 LOFC 230-340 KSC- - - A L C - 3 4 I N T E R F A C E S / C GSE T O UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO 'I RN-CCBD NO IRN-CCBD NO IRN-CCBD - C R I T + I N T F LOC S / C ENTERED ENTERED ENTERED L C 3 4 S E R V STRUCTURE-GSE-LAUNCH ICD-CCBD 201-66-140 NO IRN-CCBD ENTERED FLD SYS .. VEHICLE 06-18-65 LO-FC 200-340 K SC- �. A P O L L O I N T E R F A C E ,CONTROL, ,DOCUMENT L O G PAGE DATE 29 J U L 66 -- --- -- J 5 DOCUMENT N U M B E R * OR R E V I S I O N N O T I C E R DOC REV 2 DOCUMENT T I T L E OR C C B D NUMBER NO I R N - C C B D - - - LO-FC 220-340 KSC-EDV-2 01-1 0-66 LO-FC 000-340 KSC-EDV 10-06-65 LO-EL 220-340 MSFC-ASTR LV ESE T O RANGE S E Q U E N C I N G L C - 3 4 ICD-CCRD 2 0 1 - 6 5 - 0 0 3 6 05-28-65 LO-EL 220-340 MSFC-ASTR L V E S E T O F A C I L I T Y AC POWER L C - 3 4 NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D 08-12-65 LOEL 220-340 MSFC-ASTR L C 3 4 P H Y I N T F S - I B S T A G E T O HOLDDOWN ARM I C D - C C B D 201-66-139 A L V E S E T O I N S T R S Y S + RECORDERS ICD-CCBD 2 0 1 - 6 5 - 0 0 3 8 - PREPARING I N T E R F A C E AREAS CENTER OR C E I N U M B E R S A C T I V " 'Y 09-29-65 A L V E S E TO F A C I L I T Y C A B L I N G L C - 3 4 I C D - C C B D 201-66-0344 NO I R N - C C B D E N T E R E D - , 0 2 - 1 8-66 LO-EL 220-200 NSFC-ASTR MSFC COUNT C L O C K T O K S C T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 3 9 I R N - C C B D 201-65-0039 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 06-08-65 LO-EL 200-240 MSFC-ASTR L V E S E T O K S C D A T A MEASUREMENTS I C D - C C B D 201-66-0146 IRN-CCBD 20 1-66-0146 12-1 5-65 LO-EL 220-340 MSFC-ASTR 05-28-65 LO-EL 220-340 MSFC-ASTR --L V t ENTERED A L C 3 4 PAD AREA/GSE-LIV I C D - C C B D 201-66-138 - SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO D A YR CODE 28 --- E S E T O WATER D E L U G E S Y S T E M - . �-\. -. APOLLO INTERFACE CONTROL DOCUMENT LV:.v -y DATE 2 9 JUL 6 6 -- --- -- -2' (. -)! ! 4. c ; H ' 1 D S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E - --- - ------.---??* , , R DOC REV DOCUMENT T I T L E OR CCBD NUMBER ---------- --- ----------------.................... ICD-CCBD IRN-CCBD 1 SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR M O DA YR CODE PRE INTERFACE AREAS CEN OR C E I NUMBERS ACT 201-65-0040 201-65-0040 -. D 651CD5740 3 I 0 SAT I B P I P C R I T 4 I N T F LOC APS PPOP ICD-CCBD 2 0 1 - 6 6 - 1 4 2 02-1 1-66 LO-PG 220-347 MSFl 07-26-65 LOPG 220-340 K S%- 11-1 0 - 6 5 LO-FA 040-347 M S FC 11-10-65 LO-FA 040-347 HS FC A PHY I C D PNEUMATIC CONSOLE 0 S V - 4 8 - 4 3 2 / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 8 10-25-65 LO-FA 220-347 KSC- A PHY I C D PNEUMATIC CONSOLE OSV-48-433 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 03-02-66 LO-FA 220-347 KSC- A PHY I C D PNEUMATIC CONSOLE O S V - 4 8 - 4 3 6 / 1 8 ICD-CCBD 201-66-0)3? 03-02-66 - PHY I C D S - I V B APS PORTABLE VALVE BOX A PHY I C D APS MODULES ON L A U VEH/SAT ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 ERN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A P I P I N G CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 I RN-CCBD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 I RN-CCBD 20 1 - 6 6 - 0 2 8 1 IB APS PMEU U N I T S / I B LO-FA 220-347 KSC-: �APOLLO INTERFACE CONTROL,, DOCUMENT LOG DATE 2 9 J U L 66 AS -- --.. -- D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E . -. DOC REV _ -------------------- --R 3 J 65LCD5883 R CONT. DOCUMENT T I T L E OR CCBO NUMBER -------o------------------------------- IRN-CCBD - 204 .--...-- 201-66-028 IAOl PAGE SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE -------- -------- --.---- 30 --- PREPARING INTERFACE AREAS CENTFOR C E I N U M B E R S ACTIL * Y - ----------POP- ---------- 1 04-12-65 LO-FA 220-347 A P I P I N G C R I T E R I A S I V B STAGE PNEU SUP SYS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 02-04-66 LOFA 040-347 HSFC-EDV A PHY I C D AFT UMB SWING ARM NO 2 S - I V S NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 WS FC-K-DT A PHY I C D FWD UMB S W I N G ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66. LO-FA 040-347 A PHY I C D I U UMB SWING ARM NO 3 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-15-66 LOFA 090-347 MSFC-K-DT 08-02-65 LO-FA 010-347 KSC-P+VE 1 - . PHY I C D HEAT EXCHANGER D S V - 4 8 - 4 3 8 / 1 8 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 7 PHY I C D UMB NO IRN-CCBD NO IRN-CCSD NO IRN-CCSD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PHY I C D UMB CONN S - I B / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED KSC-K-DT -.- MSFC-DT\ I (SH C MAST111 SH H A S T I V �A P O L L O INTERFACE CONTROL DOCI!NENT DATE 2 9 JUL 66 -- --- AS -- 2 0 4 CONT. ----- C ' H a G i --- D DOCUMENT N U M B E R p OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER ------------------ --- ....................................... NO IRN-CCBD NO IRN-CCBD * J 65fCD5890 1 9 R - SCHED ACTUAL R E 1 DATE R E L DATE PANEL MO DA YR MO DA YR CODE PREFA INTERFACE AREAS CENTEI OR C E I NUMBERS ACTIV -------- ------- ------ -------------- -----. ENTERED ENTERED PHY I C D OBAT T A I L LOX UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 4 08-02-65 LO-FA 010-347 KSC-Pd P H Y S I C A L I f D BOAT T A I L FUEL UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 08-02-65 LO-FA 010-347 KSC-P- 08-02-65 10-FA 010-347 KSC-P- PWY I C D BOAT TAIL CON0 UMBLS S - 1 8 / 1 6 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 08-02-65 LO-FA 010-347 KSC-P+ A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 201-66-0282 03-02-66 LO-FA 220-347 KSC-P4 12-30-65 LO-FA 220-347 HS FC-K 1 - - J 65ICD5895 R LA R 2 R 3 LOG PHY I C D UMB NO IRN-CCBD NO fRNGCCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B FWD {SW ARM = 1 1 ENTERED ENTERED ENTERED ENTERED ENTERED A PHY I C D S - I V B / I U COOLING U N ~ T / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 �. APOLLO INTERFACE CONTROL DOCUMENT LOG D A T E 2 9 J U L 66 -- D S AS --- .-- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV CONT. ICD-CCBD PAGE SCHED REL DATE MO DA Y R DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD - 204 ----- ACTUAL R E L DATE PANEL MO DA YR CODE -- PREPARIN( INTERFACE AREAS CENTER OR CEX NUMBERS A C T ITY - 201-66-0144 2 0 1-66-0238 PHY I C D VACUH MONITORING CONSOLE SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 4 1 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 5 IB 01-10-66 LO-FA 040-347 MSFC-EDV 12-1 6-65 LO-FA 290-347 KSC-P+VE 02-08-66 LOFC 230-370 KSC A PHY I C D I U COOLING U N I T L C 3 4 ALTERNATE NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 A PHY INTF CONT DWG Ill FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 - LC 3 7 HAZARD PROOFING S / C NO IRN-CCBD ENTERED . r - LC/34/37/39 A S/C - A.C. T I M I N G + COUNTDOWN D I S T POWER REC- LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD + CONN SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED L C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED VERT STOP F O R L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 09-22-64 LO-FC 230-340 11-29-65 LOFC 230-347 KSC-EDV-; 10-01-64 LOFA 230-340 MSC-FO-H, �-- APOLLO INTERFACE CONTROL DOCUMENT L O G DATE 29 J U L 6 6 -- --- -- i ';i D G , SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MU DA YR CODE C H 5 --- - DOCUMENTNUMBER, D R R E V I S I O N NOTICE .................... J 65ICD8304 J 65ICD8308 1 1 J 651CD8311 DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ A MOCK-UP i! R DOC REV 23 AF RM 9 TO ACCESS ARM WHT RM - L C 3 4 1 3 7 S M ARM ELE CABLE + FLTR BOX I N S T NO IRN-CCBD ENTERED - C/M ACCESS ARM ADPT HOOD TO S / C a - L C 3 4 / 3 7 L/V+S/C S-IB MISALIGN, I N T F REQ 11-04-65 LOFA 100-300 MSC-I FOR SAT I f 3 VEH 07-01-65 .LO-FC 200-347 MS FC- 07-01-65 LOVC 05-07-65 LO-PG 220-347 KSC-C 02-23-66 LOPG 000-220 KSC-E 05-25-65 LO-PG 000-220 KSC-K LV PROTUBERANCES L C 3 4 / 3 7 FUNCT I / F F L D RQMTS-ECS-SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 7 IS-L/V GSE A FUNC IMTF F L U I D REQMTS GN2 SYS SAT I 8 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 - I PREPl INTERFACE AREAS CENTt OR C E I NUMBERS ACTI\ 501-66-0039 MSFC . FUNC I N T F F L U I D REQMTS GN2 SYS S A T I f 3 ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 L-66-0 1 3 2 �. APOLLO INTERFACE. CONTROL DOCUMENT LOG D A T E 2 9 JU4 66 PAGE -- --- -- b S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD A 65ICD8603 R R - 1 2 J 65ICD8701 - SCXED ACTUAL REL DATE REL DATE PANEL MO DA YR MO DA YR CODE 34'- -- PREPARING INTERFACE AREAS CENTER Y OR C E I N U M B E R S A C T I ! - -------- ------- ------ --------------- \ ;- -------y 201-66-0132 201-66-0132 i FUNC I N T F F L U I D REQMTS L H 2 SYS SAT I 0 ICD-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 05-24-65 LO-PG 000-220 KSC-K-DT FUNC I N T F F L U I D REQMTS L H 2 SYS SAT 16 ICD-CCBD 2 0 1 - 6 6 - 0 0 7 3 IRN-CCBD 201-66-0073 05-24-65 LO-PG 000-250 KSC-K-DT FUNC I N T F F L U I D REQMTS LOX SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBO 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 05-25-65 LO-PG 000-250 KSC-K-DT - FUNC I N T F F L U I D REQMTS RP-1 SYS SAT 1B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 L - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 05-25-65 LO-PG PHY I N T F RETRACTION MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 12-10-65 LO-FA PHY I C D C A L I P S C / O CONSOLE SAT I B 01-04-66 LOFA PHY TCD HAZARDOUS GAS ANALYZER SATURN 1 B ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA !&OW BAY ESE TO I N S T R U SYS + REC 02-1 1-66 LO-EL COVER " 2 220-347 WSFC-EDV (- �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 2 9 JUL 66 -- --- -- --1 i -< ': C +: H D G ; , --- - DOCUMENT N U M B E R 9 OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER ---""--' ' " ' "-"'--' --------------------------------------*,- ACTUAL SCHED REL DATE REL DATE PANEL MO DA Y R MO DA YR CODE -------- ---0--- PREPC INTERFACE A R E A S CENTE OR C E I N U M B E R S ACTIV ------ --------------- ----.= /. ICD-CCBD 501-66-0171 FLIGHT MECHANICS I C D 04-29-66 FM 000-100 , MSFC- �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE1 2 9 J U L 66 PAGE -- --- -- DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DOC REV -------------------- --- DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO D A YR CODE -------- ------ 3 PRE34R INC INTERFACE AREAS CEI 2 OR C E I NUMBERS A C T I V I T Y - -----I-----POP---------------I---------------------------- ------- B L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 2 0 1 - 6 6 - 0 1 7 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 7 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 5 B L A U VEH/SPACECRAFT FUNCTIONAL REQ ICD-CCBD 2 0 1 - 6 6 - 0 1 4 5 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 5 IRN-CCBD 201-66-0175 i - I N S T U N I T T O SPACECRAFT PHYS REQ IRN-CCBD 2 0 1 - 6 6 - 0 1 9 9 IRN-CCBD 2 0 1 - 6 6 - 0 1 9 9 SPA-CECRAFT TO Q-BALL IRN-CCBD 2 0 1 - 6 6 - 0 1 9 6 IRN-CCBD 2 0 1 - 6 6 - 0 1 9 6 A ENVELOPE L E M / S - I V B / I U ICD-CCBD 2 0 1 - 6 6 - 0 1 6 3 PHYS REQ CLEARANCE PHYS I C A L 8 SATURN/APOLLO FREQ PLAN ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 . EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 L V TO SCO14 I N S T R AND COHM INTERFACE ICD-CCBD 2 0 1 - 6 6 - 0 0 5 7 IRN-CCBD 2 0 1 - 6 6 - 0 0 5 7 IRN-CCBD 2 0 1 - 6 6 - 0 0 5 7 IRN-CCBD 2 0 1 - 6 6 - 0 0 5 7 08-17-65 IC 000-100 MS FC-ASTR �I e IAnl A P O L L O I N T E R F A C E CONTROL DOCUMENT LOG 2 '; PAC -- --- -- DATE 29 JUL 66 C : H G 3 S j --- - DOCUMENTNUMBERo OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- --------------------,,-,,,,,,-------,,,,,,,,- A 13M65000 B D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 A 131465205 - A 16331-63A107350 - i SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO D A YR CODE -------- I B ONBOARD EDS -o------ ------ --------------- ----- CS 000-100 MSFC C-S 000-100 MS FC- 03-18-65 EI 230-300 MS FC 08-12-65 EI 300-100 HSC 08-06-65 EI 220-250 MS FC- 04-09-65 EX 210-220 MSFC- L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 12-15-65 EI 220-250 HSFC- LV ESE/LAUNCH EOUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 12-16-65 €1 220-210 -MS FC- SAT I 6 LV E S E TO APOLLO S / C E S E ICD-CCBD 2 0 1-65-0045 IRN-CCBD 2 0 1 - 6 6 - 0 1 7 7 11-22-65 EI 220-230 MSFC- EDS L I M I T S E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 08-06-65 PREPd I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV 10-15-66 COMP I N T F ." % A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 COKP I N T E R F A C E A L V E S E TO PROPELLANT SYS AND ECS IRN-CCBD 2 0 1 - 6 6 - 0 1 7 9 - LV NO NO NO NO NO NO NO - A 40M05428 R 1 - ESE TO LAUNCH EQUIPMENT IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 2 9 J U L 66 PAGE -- --- -- D S DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD IRN-CCBD MSFC-ASTR 09-30-66 + APOLLO S C - 0 1 4 A DES OF SATURN S A - 2 0 5 ICD-CCBD 2 0 1 - 6 6 - 0 2 2 1 - - E L E C XNTFC EDS CHECKOUT SCHEMATICS - DEF -- DEF PREP" IMG I N T E R F A C E AREAS CEMI. , OR C E I NUMBERS ACTIVITY 201-66-0315 201-66-0333 201-66-0333 A DEF S A - 2 0 5 AND S C - 0 1 4 NO IRN-CCBD ENTERED - SCHED ACTUAL R E L D A T E R E L D A T E PANEL MO DA YR MO DA YR CODE -3--8 05-09-66 EDS EI MSFC C-S MS FC-ASTR SAT 1 8 I U CMD SYS G S E / L C - 3 4 + L C - 3 7 07-1 5-66 IC SAT I B SRSC T E S T ENCOD/LC-34+LC-37 07-1 5 - 6 6 IC 280-290 MSFC-ASTR 280-290 MSFC-ASTR , DEF SRSC DECODER/LC-34 4 LC-37 INTF 07-1 5 - 6 6 IC 280-290 MSFC-ASTR DEF S A T I B SRSC I N 0 P A N E L / L C - 3 4 + L C - 37 07-15-66 IC 280-290 MSFC-ASTR DEF SAT I B SRSC CODE PLUG/DECODER INTF 07-1 5-66 IC SEE-DWG NSFC-ASTR 03-1 5-66 I?-NF 040-090 MSFC I C D SATURN I B / V CONTROL R A T E GYRO P K G .-ED B LC34 S I T E PLAN-FACILITY-TO S/C ESE/GST 07-23-65 LOFC 230-340 KSC-EDV-2 A L C 3 4 DATA T R A N S M I S S I O N SYS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED ( W I V E BAND) 09-24-65 LOFC 230-340 KSC-€DV-2 02-02-65 LO-FC KSC 11-2 5 - 6 4 LOFC I<SC-F A L C 3 4 F A C I L I T Y INST, - C A B L I N G SYSTEM L C 3 4 AC E L E C T POWER SYSTEM �APOLLO I N T E R F A C E CONTROL DOCUMENT LO:; DATE 29 J U L 6 6 AS 205 CONTo C H I) G 5 --- DOCUMENTNUMBERo OR R E V I S I O N N O T I C E 65 I C D 5 0 0 7 * 4 A 65ICD5050 f? 6 , PAGE SCHED ACTUAL REL D A T E R E L DATE PANEL MO DA YR MO DA YR CODE DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ A 65ICD5006 1A 0 1 -------- -------- ------ PREPAF I N T E R F A C E ARE S CENTER OR C E I NUMBERS ACTIVI --a----------- ------ A L C 3 4 SAT I 8 S / C TRANPO ROUTES 03-1 5 - 6 5 LOFC 230-340 KSC-F - 12-02-65 LOFC 230-340 KSC-EC 02-28-66 LOEL 230-340 KSC 08-11-65 LOEL 210-340 KSC-LV 09-14-65 LOPG 100-530 USC-ED ESE/GSE 06-03-65 LOFC 230-340 KSC-F B L C 3 4 S E R V I C E STRUCTURE -TO S / C ESE/GSE 07-23-65 LOFC 07-23-65 LOFC 230-340 'KSC-EDV LC-34 HAZARD PROOFING S / C ESE/GSE D LC 3 4 CSM E S E TO F A C C A B L I N G NO IRN-CCBD ENTERED A L C 3 4 HAZARD PROOF M O N I T O R I N G F O R S / C NO IRN-CCBD ENTERED - P I P C R I T + f M T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD E N f ERED GSE F L D SYS L C 3 4 SS - B L C 3 4 LAUNCH CONTROL CENTER-S/C NO NO NO NO NO NO NO NO NO NO NO NO NO NO IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRM-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED f NTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED A ' L C 3 4 PAD AREA T O S/C' ESE/GSE . ' �APOLLO INTERFACE CONTROL DOCUMENT LOG IA 0 1 --40 PAGE D DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV _ -___________-_-----........................................ S R R R R DOCUMENT T I T L E OR CCBD NUMBER NO NO NO NO 3 4 5 6 IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD SCHED ACTUAL REL DATE R E L DATE PANEL MO DA Y R MO DA YR CODE -------- -------- ------. PREPARING - INTERFACE A R E A S CENTER OR C E I N U M B E R S ACTIVITY ----. ---------.-....-.PI- I - ENTERED ENTERED ENTERED ENTERED J 65ICD5366 C L C 3 4 PAD AREA MECH GSE 09-16-64 LOFC 230-340 A 65XCD5367 - FUNCT INTERFACE REQ ECS L C 3 4 S/C-GSE 01-27-65 LOPG 100-340 FUNC I N T F REQMTS GHE L C 3 4 S / C GSE 09-1 5-65 LOPG 100-230 KSC-EDV FUNC XNTF REQMTS GN2 L C 3 4 S / C NO IRN-CCBD ENTERED GSE 09-15-65 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-15-65 LOPG 100-230 KSC-EDV 04-05-66 LOFC 230-340 KSC-EDV A 65ICD5368 A 65ICD5370 - A L C - 3 4 INTERFACE S / C GSE TO UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - C R I T + I N T F LOC S / C ENTERED ENTERED ENTERED L C 3 4 SERV STRUCTURE-GSE-LAUNCH ICD-CCBD 2 0 1-66-140 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 PAD AREA/GSE-L/V F L D SYS VEHICLE . KSC-F ' KSC-K-DT , 09-1 5 - 6 5 LOFA 230-340 KSC-EDV 06-1 8-65 LO-FC 200-340 KSC-P+VE 09-29-65 LO-FC 220-340 KSC-EOV-2 �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D4T.E 2 9 J U L 66 -- --- -- -j -, : ' H G 3 -S .- --. \ -i DOCUNENTNUMBERp OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ...................................... --------------I---- ICD-CCBD - F 65ICD5561 1 ------ --------------- ---I---I-- .=,---. L C 3 4 PHY I N T F S - I S STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 1 3 9 01-10-66 LO-FC 000-340 KSC-I 10-06-65 LO-EL 220-340 MS FC- L V E S E TO RANGE SEQUENCING L C - 3 4 ICD-CCBD 2 0 1 - 6 5 - 0 0 3 6 05-28-65 LO-EL 220-340 MS FC- LV NO NO NO 08-12-65 LOEL 220-340 HSFC- 02-18-66 LO-EL 220-200 MS FC- MSFC COUNT CLOCK TO KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 06-08-65 LO-EL 200-240 MS FC- L V E S E TO KSC DATA MEASUREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 4 6 IRN-CCBD 2 0 1-66-0146 12-15-65 LO-EL 220-340 MSFC- L V ESE TO HATER DELUGE SYSTEM ICD-CCBD 2 0 1 - 6 5 - 0 0 4 0 IRN-CCBD 2 0 1 - 6 5 - 0 0 4 0 05-28-65 I A 65ICD5602 \ I PREn I N T E R F A C E A R E , S CENT OR C E I NUMBERS ACTI' 2 0 1-66-138 A L V ESE TO F A C I L I T Y C A B L I N G L C - 3 4 ICD-CCBD 2 0 1 - 6 6 - 0 3 4 4 NO IRN-CCBD ENTERED 2 SCHED ACTUAL REL DATE R E L DATE PANEL HO DA YR MO DA YR CODE R k R - L 2 3 E S E TO F A C I L I T Y AC POWER L C - 3 4 IRN-CCBD ENTERED I RN-CCBD E N f €RED IRN-CCBD ENTERED -\ A L V ESE TO I N S T R SYS + RECORDERS ICD-CCBD 2 0 1 - 6 5 - 0 0 3 8 - 1 -. A 651CD5605 R - 1 - LO-EL 220-340 HSFC- �* APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl PAGE DATE 2 9 J U L 66 -- I ; --- -- DOCUME:laT NUMBER, OR R E V I S I O N N O T I C E DOC REV . SCHED ACTUAL R E L D A T E R E L DATE PANEL MD DA YR MO D A YR CODE DOCUMENT T I T L E OR CCBD NUMBER B SAT II3 P I P C R I T + I N T F LOC APS PPOP ICD-CCBD 1 65ICD5741 - 42(- --- .- PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVT'Y - ,'\.. 0 2 - 1 1-66 LO-PG 220-347 HSFC-EDV 07-26-65 LOPG 220-340 KSC-P+VE 11-10-65 LO-FA 040-347 MSFC-EDV 11-10 - 6 5 LO-FA 040-347 MSFC-EDV . 10-25-65 LO-FA 220-347 KSC-K-DT . 03-02-66 LO-FA 220-347 KSC-K-DT 03-02-66 LO-FA 220-347 KSC-K-DT 04-12-65 LO-FA 220-347 KSC-K-DT 201-66-142 PHY I C D S - I V B APS PORTABLE V A L V E BOX I A PHY I C D APS MODULES ON L A U V E H / S A T ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 3 I RN-CCBD 2 0 1-66-0239 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A P I P I N G CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 IB APS PNEU U N I T S / I B A PHY I C D PNEUMATIC CONSOLE DSV-4B-432/ ICD-CCBD 2 0 1 - 6 6 - 0 2 8 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 8 IB A PHY I C D PNEUMATIC CONSOLE D S V - 4 0 - 4 3 3 1 CD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 A PHY I C D PNEUMATIC CONSOLE D S V - 4 B - 4 3 6 / ICD-CCBD 2 0 1 - 6 6 - 0 1 3 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 - P H Y I C D HEAT EXCHANGER D S V - 4 B - 4 3 8 / 1 8 IR - - < i .1 �APOLLO I N T E R F A C E CONTROL DOCUMENT Lob DATE 2 9 JUL 66 -- --- -- C H G D S DOCUMENT N U M B E R 9 OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD B 65ICD5884 R 2 R 3 , ACTUAL SCHED R E L D A T E R E L DATE PANEL MO OA YR MO DA YR CODE -------- --P-CQ-- PREP I N T E R F A C E AREAS CENTr OR C E I NUMBERS ACTI' ------ -------------- ----. 201-66-0287 201-66-0287 A P I P 1 NG C R I T E R I A S I V B STAGE PNEU SUP SYS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 02-04-66 LOFA 040-347 MSFC- A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 MSFC- 0 1 - 2 1-66 LO-FA 040-347 MSFC- 03-15-66 LOFA 090-347 MSFC- 08-02-65 LO-FA Ql0-347 - use- 08-02-65 LO-F A 010-347 'KSC-I A PHY I C D FWD UMB S H I N G ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 . NO IRN-CCBD ENTERED . 1R;d-CCBD 2 0 1 - 6 6 - 0 2 9 0 A PHY I C D I U UMB SWING ARM NO 3 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 - - PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO I.RN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED (SH C M A S T I I ) SH H A S T I V . PHY I C D 0 8 A T T A I L LOX UMB S - I B / I B �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 JUL 6 6 D S - DOCUMENT NUMBER* OR R E V I S I O N N O T I C E AS DOC REV 205 CONTa DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ ICD-CCBD IRN-CCBD J 65ICD5891 R 1 . - IA 0 1 PAGE SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE -------- ------- ------ 4 L PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTIVITY - -O.-p--QP--L-PI-P- P--- ---- 201-66-0284 201-66-0284 P H Y S I C A L I C D BOAT T A I L FUEL UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 08-02-65 LO-FA PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD 08-02-65 LO-FA P H Y . I C D BOAT T A I L COND UMBLS S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 08-02-65 LO-FA 0 10-347 KSC-P+VE A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 03-02-66 LO-FA ' 220-347 KSC-P+VE A PHY 1CD S - I V B / I U COOLING U N I T / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 01-07-66 LOF A 220-347 KSC-P+VE 12-30-65 LO-FA 220-347 MSFPK-DT 1 - - - CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED FWD (SW ARM = 1 1 P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 -- PHY I C D VACUM MONITORING CONSOLE SAT I B . . 01-10-66 LO-FA 040-347 MSFC-EDV �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 3 DATE 2 9 JUL 66 -- 3 w* \ ! -\ I e H G - D S --- -- DOCUMENTNUMBERo OR R E V I S I O N N O T I C E - ------------------- DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ ICD-CCBD IRN-CCBD J 6SICD5898 3 9 7* I --. . i 7 R R 2 3 .- - k>, J ------ ---- ---------------. 12-16-65 LO-FA KSC- 02-08-66 LOFC KSC TIMING + COUNTDOWN DXST 09-22-64 LO-FC + CONN 11-29-65 LOFC 10-01-64 LOFA LC 37 HAZARD PROOFING S / C NO IRN-CCBD ENTERED LC/34/37/39 A S/C 2 -------I 20 1-66-0141 201-66-0285 A PHY I N T F CONT DWG IU FLOW CONT V A L V E BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 1 E 65ICD6007 R 1 -_------ PREF I N T E R F A C E AREAS C E N T OR C E I NUMBERS ACTI A PHY I C D I U C O O L I N G U N I T L C 3 4 ALTERNATE NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 , J 651CD5899 R SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE A,C, POHER REC. LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCSD SM SWG ARM UM8 D I S C A 1 4 0 1 9 . ENTERED ENTERED L C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED V E R T STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED HSC+ J 65IC08304 A MOCK-UP 23 AFRM 9 TO ACCESS ARM WHT RM KSC-l J 65 I C D 8 3 0 8 - SM ARM ELE C A B L E + F L T R BOX I ~ S T KS C-l LC34/37 �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 AS -- --- -- O S - DOCUMENT NUMBER, O Y R E V I S I O N NOTICE DOC REV -------------------- --R 1 ----, - I PAGE SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE -------- -------- ------ 46 --- PREPARING I N T E R F A C E AREAS CENTER ACTIVITY OR C E I NUMBERS - ------I-------------------------------- ENTERED C/M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 MSC-EDV M I S A L I G N - F O R SAT 1 8 VEFI 07-01-65 LO-FC 200-347 HSFC-P+VE - 07-01-65 LOVC 05-07-65 LO-PG 220-347 KSC-DP. 02-23-66 LOPG 000-220 KSC-EDV FUNC I N T F F L U I D REQMTS GN2 SYS SAT 1 B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBO 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 05-25-65 LO-PG 000-220 KSC-K-DT FUNC I N T F F L U I D REQMTS LH2 SYS SAT I 8 05-24-65. LO-PG 000-220 KSC-K-DT LC34/37 S-I0 L/V+S/C L V PROTUBERANCES L C 3 4 / 3 7 FUNCT I / F F L D RQMTS-ECS-SAT ICD-CCBD 201-66-0127 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 7 IB-L/V GSE A FUNC I N T F F L U I D REQMTS GN2 SYS SAT I 0 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 - CON?. GOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD - 205 501-66-0039 MSFC �I APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 JUL 66 ) -- --- -- ./ .) c ' H G .J - O S OOCUMENTNUMBERF 3R R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -------------------- --- ....................................... ICD-CCBD IRN-CCBD IRN-CCBD > > A 65ICD8604 R - 1 A 651CD8605 R R a - L 2 - .. F 65ICD8700 - j - A 80M90205 SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE PREP, I N T E R F A C E AREAS CENTi OR C E I NUMBERS A C T I \ 201-66-0128 201-66-0128 201-66-0128 FUNC I N T F F L U I D REQMTS L H 2 SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 0 7 3 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 3 05-24-65 LO-PG 000-250 KSC-)l FUNC I N T F F L U I D REQMTS LOX SYS S A T I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 05-25-65 LO-PG 000-250 KSC-F FLUID REQMTS RP-1S Y S S A T IB 201-66-0131 201-66-0131 2 0 1-66-0131 05-25-65 LO-PG 000-250 KSC-C 12-10-65 LO-FA 110-300 KSC-E PHY TCD C A L f P S C / O CONSOLE SAT I B 01-04-66 LOFA 220-347 MSFC- PHY I C D HAZARDOUS GAS ANALYZER SATURN I B ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA 220-347 MSFC- 02-11-66 LO-EL 220-290 MS FC 04-29-66 FM 000-100 HS FC- FUNC' INIF ICD-CCBD IRN-CCBD I RN-CCBD PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 LOW BAY ESE TO I N S T R U S Y S ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 B F L I G H T MECHANICS I C D + REC COVER - �APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE D A T E 2 9 J U L 66 -- --- -- 0 DOCUMENTNUMBERI 5 OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE 0------9 - L A U VEH/SPACECRAFT --Q. ---- FUNCTIONAL REQ I N S T U N I T TO SPACECRAFT PHYS REQ IRN-CCBD 2 0 1 - 6 6 - 0 1 9 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 9 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 9 1 CLEARANCE P H Y S I C A L 000-100 HSFC-P+VE 000-1 00 MSFC EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 08-17-65 IC 000-100 MSFC-ASTR L V TO SCBP30 I N S T R + COMM INTERFACE ICD-CCBD 2 0 1 - 6 6 - 0 0 6 6 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 9 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 4 6 08-02-65 IC 000-100 HSFC-ASTR 000-100 PIS FC 230-300 MSFC B D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 - - INTERFACE AREAS C E N T E R OR C E I NUMBERS ACTI1'TTY -------- ------ -------------- B SATURN/APOLLO FREQ PLAN ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - PREPARING L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 2 0 1 - 6 6 - 0 0 6 0 IRN-CCBO 2 0 1 - 6 6 - 0 8 1 6 A ENVELOPE L E M / S - I V B / I U ICD-CCBD 20 1 - 6 6 - 0 1 6 1 - 4E --- ELEC ICD\ACE S/C-L/V I B ONBOARD EDS COMP I N T F �1 APOLLO I N T E R F A C F CO&;RL)L 2. DATE 2 9 . J U L 66 AS -- --- -- 206 ----- CLINT, ! c . j H G -- D S . DOCUMENTNUMBERI OR R E V I S I O N N O T I C E A 16331-63A107393 R ) 1 A 401Yi05419 1 R + Q 9 - 1 A 40M05435 R R - - 1 2 +++ A 4 0 M L 1 8 4 6 - _ _ _ _ _ _ _ _ _ _ _ COMP I N T E R F A C E 300-100 MSC L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 IRN-CCBD 201-66-0094 220-250 MS FC- LV E S E / L A U N C H EQUIPMENT ICD-CCBD 20 f - 6 5 - 0 0 4 8 IRN-CCBD 201-66-0095 2 2 0 - 2 10 MSFC- SAT I B L V E S E T O APOLLO S / C E S E ICD-CCBD 2 0 1 - 6 5 - 0 0 5 3 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 7 220-230 MS FC- EI 220-230 MSFC- 03-11-66 E-I 000-1 00 MS FC- 11-29-65 CS 000-100 MSFC- EI 000-220 MS FC SC E S E TO L V E S E ( A L T E R N A T E M I S S I O N ) 05-01-66 A DEF S A - 2 0 6 9 B P - 3 0 E L E C T R I C A L I N T E R F A C E IRN-CCBD 2 0 1 - 6 6 - 0 2 1 8 A 40M37527 * A 40M37539 - - D E S C R I P T I O N SATURN 206 APOLLO B P 3 0 EDS EDS CHECKOUT SCHEMATICS DES OF SATURN S A - 2 0 6 ICD-CCBD I A 401.137677 - ------ --------------- ----- -------_ PREP4 INTERFACE A R k A S CENTE OR CEI NUMBERS ACTIV 5 0 1-66-0085 A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 I A 4OM05417 , DOCUMENT T I T L E OR CCBD NUMBER _ _ _ _ I _ _ _ _ _ ~ _ ~ ~ _ _ _ _ _ ~ ~ _ ~ O _ ~ ~ ~ _ ~ ~ _ ~ _ _ _ _ _ _ ~ _ _ _ P_ _ _ _ 1 ' ___ SCHEO LCTUAL R E L O A T ; A E L D A T i PANEL MO DA Y R MO PA Y R CODE . ICD-CCBD I ' DOC REV I.bC 1 DCSUMENT L C 11-30-66 + APOLLO S C - 1 0 1 EDS 03-11-66 C-S 000-100 - MS FC- ELECTRICAL INTERFACE 02-16-66 E-I 000-100 MSFC- 201-66-0182 DEF S A - 2 0 6 + S C - 1 0 1 ICD-CCBD 2 0 1 - 6 6 - 0 0 5 3 6 . �APOLLO INTERFACE CONTROL DOCUMENT LOG D A T t 2 9 JUL 66 AS -- --- -- O DOCUMENT NUMBER, OR R E ? I S I O N NOTICE DOC REV _ -------------------- --S - 206 ----- IA 0 1 CONTe PAGE SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO D.A YR CODE DOCUMENT T I T L E OR CCBD NUMBER 50 --- PREPARING - INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y -------- ------- ------ --------------- ---- ---- -----------------------------,----------- DEF SAT 1 6 I U CMD SYS GSE/LC-349LC-37 07-1 5-66 IC 280-290 HSFC-ASTR DEF SAT I B SRSC TEST ENCOD/LC-34+LC-37 07-1 5-66 IC 280-290 HSFC-ASTR 07-15-66 IC 280-290 MSFC-ASTR DEF S A T I B SRSC I N D PANEC/LC-34+LC-37 07-15-66 IC 280-290 MSFG-ASTR DEF SAT I B SRSC CODE PLUG/DECODER 07-1 5-66 IC SEE-DUG MSFC-ASTR 03-1 5-66 M-NF 100-230 KSC-EDV DEF SRSC DECODER/LC-34 I C D SATURN I B / V + LC-37 Ili' INTF CONTROL RATE GYRO PKG P I P C R I T 4 I N T F LOC S/C NO 1 RN-CCBD ENTERED F L D SYS L C 3 4 SS 09-14-65 LOPG - FUNC I N T F REQMTS GHE L C 3 4 S I C GSE 0 9 - 1 5-65 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GN2 L C 3 4 S/C NO IRN-CCBD ENTERED GSE 09-15-65 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV 04-05-66 LOFC 230-340 KSC-EDV 230-340 KSC-EDY 220-347 WSFC-EDV A L C - 3 4 INTERFACE S/C GSE TO UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD C R I T 4 I N T F LOC S / C ENTERED ENTERED ENTERED F L D 5:'s 8 SAT I B P I P C R I T + I N T F LOC APS PPOP 02-1 1-66 LO-PG �'3 -A APOLLO I N T E R F A C E CON'r 2c)r 3 DATE 29 J U L 6 6 -- --- -- c ! H G --, 3- D S DOCUMENTNUMBERp OR R E V I S I O N N O T I C E - .................... DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ ICD-CCBD , ACTUAL SCHED R E L DATE R E L DATE P A N E L MO DA YR MO DA YR CODE DOC REV 7 A PHY I C D APS MODULES ON L A U V E H / S A T ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 IS APS PNEU U N I T S / I B A PHY I C D PNEUMATIC CONSOLE D S V - 4 8 - 4 3 6 / ICD-CCBD 2 0 1 - 6 6 - 0 2 3 7 IRN-CC8D 2 0 1 - 6 6 - 0 2 8 1 * 1* -) 3 65ICD5883 R - 1 8 05ICD5884 - IB - - - 11-10-65 LO-FA 040-347 MSFC 11-1 0 - 6 5 LO-FA 10-25-65 LO-FA 220-341 KSC- 03-02-66 LO-FA 220-347 KSC- i 220-347 I6 PHY I C D HEAT EXCHANGER D S V - 4 8 - 4 3 8 / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 7 IRN-CCBD ------ 201-66-0288 201-66-0288 A PHY I C D PNEUMATIC CONSOLE D S V - 4 6 - 4 3 3 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 j --as--- - A PHY I C D PNEUMAT XC CONSOLE D S V - 4 0 - 4 3 2 / ICD-CCBD IRM-CCBD -------- PREF I N T E R F A C E AREP5 C E N 7 OR C E I NUMBERS ACT! 201-66-142 A PIPING CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 I RN-CCBD 20 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 s IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 \'- OOCUMENT L v l b 04-12-65 LO-FA 02-04-66 LOFA 201-66-0287 A P I P I N G C R I T E R I A S Z V S STAGE PNEU SUP S Y S 220-347 KSC- -. KSC- �APOLLO INTERFACE CONTROL DOCUMENT LOG D 5 PAGE 2 9 JUL 6 6 ---- -- JATE DOCUMENTNUMBERI OR R E V I S I O N N O T I C E DOC REV - ------..------------- -I- DOCUMENT T I T L E OR CCBD NUMBER ........................................ NO 1RN-CCBD NO IRN-CCBD J 65ICDS886 R R J. 2 SCHED ACTUAL REL DATE R E 1 DATE PANEL MO DA YR MO D A YR CODE -------- 52 -- PREPARING - INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y ------ -------------- --I---- ----r------ ENTERED ENTERED A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 MSFC-K-DT A PHY I C D FWD UMB SWING ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA 040-347 NSFC-DT A PHY I C D I U U M B S U I N G ARM NO 3 NO IRN-CC8D ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5 - 6 6 LOFA 090-347 HS F C-K-DT 08-02-65 LO-FA 0109347 KSC-P+VE 08-02-65 LO-FA 010-347 KSC-P+Vt 08-02-45 LO-FA 010-347 KSC-P+VE - - PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCSD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I S / I B ENTERED ENTERED ENTERED ENTERED PHY SH M A S T I V ICD O B A l T A I L L O X UMO S - I B / I t 3 ICD-CCBD IRN-CCBD - (SH C M A S T I I ) 201-66-0284 2 0 1-66-0284 P H Y S I C A L I C D BOAT T A I L FUEL UPlB S - 1 8 / 1 8 - �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G 7 J AS DATE 29 J U L 6 6 206 CONT, , 7: H ? 7 d I 1 m 3 C * * 9 Q 2 , * ** 0 S DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E R DOC REV J 65ICD5892 R 1 R 2 R 3A R 4 R 5 - SCHEIJ ACTUAL R E 1 DATE R E L DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD 1 P. 201-66-0278 201-66-0278 PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED FWD I S H ARM = 1 ) 010-347 K S C- 010-347 KSC-; LO-FA 220-341 KSC- 01-07-66 LOFA 220-347 KSC- 12-30-65 LO-FA 220-347 M S FC 08-02-65 LO-FA 08-02-65 LO-FA A A PHYS I C D I N S T R U N I T PNEU C O N S O L E / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 03-02-66 A PHY I C D S - I V B I I U C O O L I N G U N I T / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - - PHY ICD ICD-CCBD IRN-CCBD B O A T TAIL COND UMBLS S-IBIB 201-66-0280 201-66-0280 P I P I N G C R I f € R I A INSTRUMENT U N I T LC34-37 ICD-CCBD 2 0 1-66-0144 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 PHY ICD ICD-CCBD IRN-CCBD PREi I N T E R F A C E AREAS CENOR C E I NUMBERS ACT. VACUM MONITORING 201-66-0141 201-66-0285 CONSOLE SAT xa ' 01-10-66 LO-FA 040-347 MSFC 03-02-66 LOFA 220-347 HSFC- �IAOl APOLLO INTERFACE. CONTROL DOCUMENT L ~ G AS D A T k 2 9 JUL 66 -- --- -- U DOCUKENT NUMBER* OR R E V I S I O N N O T l C E _ .................... 5 DOC REV 206 ----- DOCUMENT T I T L E OR CCBD NUMBER -P--O---O--QI----Y-----------v---------- -P- PAGE CON?, SCHED ACTUAL REL D A T E R E L DATE PANEL MO DA Y R MO D A YR CODE -------- ------we 54 --- PREPARING - I N T E R F A C E AREAS C E N T E R OR C E I N U M B E R S A C T I ' * ' - T Y ------ --------------- a--- .---- NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 A PHY I N T F CONT DWG I U FLOW CONT VALVE LOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-16-65 LO-FA 290-347 KSC-P+VE A L C 3 7 S I T E P L A N + GENL, 08-17-65 LO-FC 230-370 KSC-EDV-2 08-25-65 LOFC 230-370 KSC-EDY-2 LC-57 S / C F A C e f N S T o CABLE SYS-PHYSICAL NO IRN-CCBD ENTERED 02-09-66 LOFC 230-370 KSC - L C 3 7 AC ELEC PWR SYS 01-28-65 LOFC 230-370 KSC-F - L C 3 7 OPNL T V SYS 03-1 5-65 LOFC , 230-370 XSC-F A L C 3 7 SAT I B S / C TRANSPORT ROUTE 03-1 5 - 6 5 LOFC 230-370 KSC-F - 02-08-66 LOFC 230-370 KSC 05-20-66 LOEL 230-370 KSC-LVO 0 2 - 1 6-66 LO-EL 230-340 HS FC-ASTR A L C 3 7 S / C DATA TRANS SYS NO IRN-CCBD ENTERED - ARRANGE S / C GSE ( W I D E BAND) LC 3 7 HAZARD PROOFING S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A F A C I L I T Y C A B L I N G L C 3 7 F O R L E M +ESM NO IRN-CCBD ENTERED - HAZARD PROOF MON FOR S I C GSE L C - 3 7 SC ESE TO DC POWER S U P L D I S T + AC I N P U T ICD-CCBD 2 0 1 - 6 6 - 0 0 7 7 �APOLLO I N T E R F A C t CONTRCL DCICuHfN l L ~ C D A T E 2 9 JUL 66 -- --- -- A .TUAL SCHED REL D A T ~RE,.. Q A T E PANEL MO DA YR M O DA YR CODE L ,h i? . S DOCUMENT NUKBERr 3R R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER 09-14-65 LOPG 100-230 KSC A L C 3 7 B S A T I B SS P I P C R I T LEM F L D SYS 05.,16-66 LOPG 230-370 KSC - 07-01-65 LOFC 230-370 KSC 08-17-65 LOFC 230-370 FUNCT I N T E R F A C E REQS ECS L C 3 7 8 S/C-GSE 03--19-65 LOPG 100-370 FUNCT I N T F REQMTS GHE L C 3 7 8 S / C GSE 05--02-66 LOPG 100-370 FUNCT I N T F REQMTS GN2 L C 3 7 8 S / C 05-02-66 LOPG 100-370 KSC- 02-09-66 LOPG 230-390 KSC- A P I P CRT'T . - -, 4 : A 65ICD6466 ? - * C 65ICD6467 * C 65ICD6468 : -? C 65 I C D 6 4 6 9 PR INTERFACE L X E ~ . .C E r OR CEI NUMBERS ACT - + I N T F LOC S / C F L D SYS L C 3 7 0 SS L C 3 7 LAUNCH CONTROL CENTER NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - S/C ESEIGSE L C 3 7 - S / C S E R V I C E STRUCTURE ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED L C 3 7 PAD B AREA ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED L C 3 9 A S / C GSE FUNC I N T F R E Q ~ G ' O X GSE K S C* - KSC- �PAGE J _ 5 DOCUMENT NUMBER9 OR R E V I S I O N NOTICE DOC REV -__,___-. ---___-___-_ --- F 65ICD6500 SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D'A YR CODE DOCUMENT T I T L E OR CCBO NUMBER - - C I - - Y P C . C . U > - P Y L ~ - - r = _ . C ~ - - - - - C - ~ P Q I P . P C _ I E A LC-37 INTERFACE S/C CZ), 1. ,--.*UU--P -------- -----c -.-----.. PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTI'!TTY - .>s>-.z--e GSE TO UMB TWR A L C 3 7 R UT PEP C R I T + I N T F LOC S i c FLC S V S NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN--5CBD ENTERED NO IRN-CCBD ENTERED - 3 7 8 PHY I N F F L E N UMB ARM C A B L E REQMTS NO IRN-GCBD ENTERED L C 3 7 SS T O L / V ESE/GSE ICD-CCBD 2 0 1 - 6 6 - 0 1 1 3 12-08-65 LC37 PAD AREA ESE/GSE-L/V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 0 2 - 1 0-66 LO-FC L C 3 7 PHY I N T F S - I 8 STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 0 1 0 1 01-1 0 - 6 6 LO-FC A 65ICD6703 -.-----;-- KSC-EDV 230-370 KSC-EDV 230-370 KSC-EDV . - -- ---- 230-370 220-370 LO-FC ---a KSC-EDV-2 . 220-370 KSC 000-370 KSC-EDV 220-210 MS FC-ASTR 220-200 MSFC-ASTR I A F A C I L I T Y CABLES L C - 3 7 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 5 - 56 --- FOR L V ESE SAT I 0 L V E S E T O RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 6 08-17-65 LO-EL L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 2 1 02-11-66 LO-EL A L V ESE/INSTRUMENTATION SYS + RECORDERS �'l APOLLO I N T E R F A C E CONTR2L GdCUMFNT L O G ) D A T E 2 9 J U L 66 PAG -- --- -- SCHED . A C T !:.Si R E L D A T E R E . 'ATE PANEL MO DA Y K MG D A YY CODE C 9 G ) ' 1101 b S - , , DCCUMENTNUMBER, OK R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER --------, ,,,-.,,.,,, .,,,,,-,, +++ A 6 5 1 C D 6 7 0 5 MSFC COUNTCLOCK TO KSC T I M I N G ICD-CCRD 20 8 - 6 5 - 0 6 5 1 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 1 - L V ESE TO K S C DATA MEASUREMENTS €3 - - , , , - , , , , , L V E S E TO WATER DELUGE SYS ICD-CCBD 2 0 1 - 6 5 - 0 0 5 2 LC/34/37/33 A S/C J 651CD8304 , > ,,, ,= . , , , , - - J 65ICD8302 R f ".-, --, --I----- TIMING A o C o POWER RECo COUNTDOWN D I S T 4 4 CONN FUNCT I N T F REQMTS ECS MC L E M S / C GSE NO IRN-CCBD SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED LC37P39 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED LC 3 4 / 3 7 / 3 9 NO IRN-CCBD ---=--.--- -... .-.-------. 03-01-66 . A PREFrr GENTE I N T E R F A C E ARt &: OR C E I NUMEEF 4CTTb - ------.=------.LC ----- LOEL 220-340 MSFC-, 07-.f 3-66 LO-EL 220-347 . MS FC- 09-22-64 LO-FC 230-340 11.-29 - 6 5 LOFC 230-347 KSC- E i 0 5 03-65 LOPG 230-300 KSC- K. 10-01-64 LOFA 230-340 MSC-FI 03.-17-65 LOFA 230-300 KSC-DE L C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP 2 3 AFRM 9 T O ACCESS ARM WHT RM �AS 206 -. - PAGE CONY- - ".- SCHED J i30CUF8ENT NUMBER, OK R E V I S I O N NOTICE _ ___- _ 5 -- _-----.I ---.I -_-. J 651CD8311 A 651CD8400 J 65ICD840h ACTUAL R E 1 DATE R E L DATE PANEL DOC REV DOCUMENT T I T L E OR CCBD NUMBER --c -L I _ .-I 2 . .--r ...<I Y e . . .-.._.'%. * -.. -.. I . _ . _ , .WY_C.._ -.-L MO DA Y R MO DA YR CODE .-- .-. ..-...- ------.. -, - ~ ~ 3 4 ~ S M3 A R 7 M ELE C A B L E c F L T R NO XRN-CCED ENTERED eox C I M A C C E S S ARM ADPT HOOD T O S / C I N r F PEQ 11-04-65 FOR S A T I 0 VEH .-< - --. ...- 58 --- PREPARING I N T E R F A C E AREAS CENTER CIR C E I NUMBERS ACTI".TY - -.-c-.CI- .i.E-...~--OOC-i P l F C i ---- 230-347 KSC-DE LSFA 100-300 HSC-EDV 07-01-65 LO-FC 200-347 MSFC-P+VE 07-01-65 LOVC GSE 05-07-65 LO-PG 220-347 KSC-DP A FUNC I N T F F L U I D REQMTS GN2 SYS SAT % B NO IRN-CCBD ENTEPED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 02-23-66 LOPG 000-220 KSC-EDV 05-25-85 LO-PG - - L C 3 4 1 3 7 L/V+S/C S-IB MESALIGN, :Nsr L V PROTUBERANCES L C 3 4 L 3 7 FUNCT Z/F F L D RQMTS-ECS-SAT ICD-CC8D 2 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 7 10-L/V FUNC I N T F F L U I D REQMTS GN2 SYS S A T I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 501-66-0039 MSFC �i APOLLO I N T E R F A C E COrVTP I C i: C U " , C V T LOG D A T E 2 9 JUL -- ) j c ti 3 S 5 AS 66 --- -- DOCUMENT NUMBER? OR R E V I S I O N N O T I C E DOC REV 206 .......-.-- A 65ICD8604 R , - Ai.1 SCHED R E L DATE REZ- D A T E P A Y E L MO DA Yh M O D A YR ::CIDE DOCUMENT T I T L E OR CCBD NUMBER ---_----- C-,. .-.----- PREPA I N T E R F A C E AREAS C E N T € OR C E I NUMBERS ACTIV ---C)-..- -I------ LO-PG 000-220 KSC-K FUNC I N T F F L U I D REQMTS L H 2 SYS SAT 1 6 ICD-CCBD 2 0 1 - 6 6 - 0 0 7 3 05-24.. 6 5 LO-PG 000-250 KSC-K FUNC I N T F F L U I D REQMTS LOX SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 0 1 RN-CCBD 2 0 1-66-0130 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 0 05-25-65 LO-PG 000-250 KSC-K 05-25-65 LO-PG 000-250 KSC-K 12-10-65 LO-FA 110-300 KSC-E PHY I C D C A L I P S C / O CONSOLE SAT I 8 01-04-66 LOFA 220-347 MSFC- PHY I C D HAZARDOUS GAS ANALYZER SATURN I 0 ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA 220-347 MSFC- L O W BAY ESE TO I N S T R U SYS + REC 02-11-66 LO-EL 2200290 MS FC 07-07-65 FM 000-100 MSFC- FUNC i N T F F L U I D REQMTS L H 2 SYS SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRM-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 IB 95. 2 4 - 6 5 1 - - FUNC I N T F F L U I D REQMTS RP-1 ICD-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 80M90206 SYS SAT 18 PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 50 1-66-0164 ICD-CCBD A PAG CONY, --- - -------------------- --- ......................................... - IPOI COVER 501-66-0171 A F M L I G H T MECHANICS PANEL I C D 4 �APOLLO I N T E R F ~ C E CONTROL DOCUMENT L ~ G I A O ~ PAGE SCHED D S - A DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV ---- ACTUAL R E L DATE R E t .DATE PANEL DOCUMENT T I T L E OR CCBD NUMBER MO DA YR MO DA YR CODE 6C --- PREPARING I N T E R F A C E AREAS CENTER OR C E I NlJMBERS A C T J ' 'TY - ----I------------------C------P---------------.POP--.QL..PY-.-=-~---- 13M06548 - L A U VEH/SPACECRAFT PROCEGURAL ICD-CCBD 2 0 1 - 6 6 - 0 0 6 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 8 7 - L A U VEH T O SPACECRAFT F U N C T I O N A L REG L A ENVELOPE L E M / S - I V B / I U CLEARANCE P H Y S I C A L ICD-CCBD 201-66-0161 - - . 000-1 0 0 MSFC-P+VE 07-07-65 MI 000-100 HSFC-P+VE 05-10-66 IC 000-100 MSFC 08-02-65 IC 000-100 HSFC-ASTR PHY REQ B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - M-I REQ I N S T U N I T T O SPACECRAFT PHY ICD-CCBD 2 0 1 - 6 6 - 0 1 6 8 NO IRN-CCSD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 1 6 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 8 SPACECRAFT TO Q-BALL ICD-CCBD 2 0 1 - 6 6 - 0 1 6 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 7 IRN-CCBD 2 0 1 - 6 6 - 0 1 6 7 12-30-65 EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 LV TO S C l O l I N S T R , + COMM. ICD-CCBD 2 0 1 - 6 6 - 0 0 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 0 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 0 6 9 IRN-CCBD 2 0 1 - 6 6 - 0 0 6 9 INTERFACE -. �APOLLO I N T E R F A C E CONTROL DUCUMENT LUG D A T E 2 9 J U L 66 -- --- -- , : SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE C H G D DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER _-- - -------------------- --- ....................................... -, B D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 13fl65207 9 A 16331-63A107350 a . - -------- -c---- -----------.s--- I B ONBOARD EDS EDS L I M I T S E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 -_.,---_-- PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV 04-1 5 - 6 7 COMP I N T F CS SEE-DWG MSFC- 03-18-65 E I 230-300 MSFC 08-12-65 €1 300-100 MSC ) A 16331-63A107393 I A 40M05417 R A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 50 1 - 6 6 - 0 0 8 3 - 1 - - t V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 4 L V ESE/LAUNCH EQUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 5 SAT 1 8 L V E S E T O APOLLO S/C ICD-CCBD 2 0 1 - 6 5 - 0 0 5 4 IRN-CCBD 2 0 1 - 6 6 - 0 3 1 9 IRN-CCBD 2 0 1 - 6 6 - 0 3 1 9 A DEF S A - 2 0 7 + S C - 1 0 1 ICD-CCBD 2 0 1 - 6 6 - 0 0 7 9 4 ESE E L E C T R I C A L INTERFACE A 40K37540 7 EDS CHECKOUT SCHEMATICS A 40M37551 - - COMP I N T E R F A C E DES SATURN S A - 2 0 7 AND APOLLO S C - 1 0 1 ICD-CCBD 2 0 1 - 6 6 - 0 0 8 0 DEF S A T I B XU CMD SYS G S E / L C - 3 4 + L C - 3 7 000-220 EDS - - MSFC 000-1 00 PIS FC-1 280-290, MSFC-A �APOLLO INTERFACE CONTROL DOCUMENT LOG AS D A T t 29 JUL 66 -- --- -- D __ S DOCUMENTNUMBERI OR R E V I S I O N N O T I C E DOC REV 207 ----- CONT, PAGE SCHED ACTUAL REL DATE REL DATE PANEL MO DA Y R MO .DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER --€ PREPARINC INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y - -------- ------- -----... 07-1 2 - 6 6 IC 07-1 5 - 6 6 IC 280-290 MSFC-ASTF DEF S A T I S SRSC I N D P A N E L / l C - 3 4 + L C - 3 7 07-15-66 IC 280-290 MSFC-ASTF DEF SAT I B SRSC CODE PLUG/DECODER 07-1 5 - 6 6 IC SEE-DWG MSFC-ASTF 03-15-66 M-NF -------------------~ ---- ----Y----P---------------I - DEF SAT I 0 SRSC TEST ENCOD/LC-34+LC-37 DEF SRSC DECODER/LC-34 + LC-37 INTF INTF I C D SATURN I B / V CONTROL RATE GYRO PUG 09-14-65 LOPG 100-230 KSC-EDV 0 9 - 1 5 - 6-.5 LOPG -- 100-230 KSC-EDV FUNC I N T F REQMTS GN2 L C 3 4 S / C GSE NO IRN-CCBD ENTERED 09-1 5 - 6 5 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV L C - 3 4 INTERFACE S / C GSE TO UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 04-05-66 LOFC 230-340 KSC-EDV 09-1 5 - 6 5 LOFA 230-340 KSC- LDV 02-11-66 LO-PG P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED F L D SYS L C 3 4 SS FUtlC I N T F REQMTS GHE L C 3 4 S/C L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD GSE C R I T + I N T F LOC S / C ENTERED ENTERED ENTERED F L D SYS SAT I B P I P C R I T + I N T F LOC APS PPOP ICD-CCBD 2 0 1 - 6 6 - 1 4 2 �APOLLO I N T E R F A C E CONTROL I.'. r!JMEhT ! OG PAGE D A T E 2 9 JUL 6 6 c H O G S --- DOCUMENTNUMBER, OR R E V I S I O N NOTICE 9 0 SCHED ACTUAL R E L DATE R E L DATE PANEL M O D A Y R M O D A Y R CODE DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ J 65ICD5840 9 DOC REV R R R 1 2 3 I PREPAF I N T E R F A C E AREAS CENTER O R C E I NUMBERS ACTIVI 11-10-65 LO-FA 040-347 MSFC-E 11-10-65 LO-FA 040-347 MSFC-E A PHY I C D PNEUMATIC CONSOLE D S V - 4 B - 4 3 2 / 1 8 ICD-CCSD 2 0 1 - 6 0 - 0 2 8 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 8 10-25-65' LO-FA 220-347 KSC-K- A PHY I C D PNEUMATIC CONSOLE D S V - 4 8 - 4 3 3 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 3 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 3 03-02-66 LO-FA 220-347 KSC-K- A PHY I C D PNEUMATIC CONSOLE D S V - 4 B - 4 3 6 / I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 03-02-66 LO-FA 220-347 KSC-K- 04-1 2 - 6 5 LO-FA 220-347 KSC-K- A PHY I C D APS MODULES ON L A U V E H / S A T 1CD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A PIPING CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 - IB APS PNEU U N I T S / I B PHY I C D HEAT EXCHANGER D S V - 4 8 - 4 3 8 / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 7 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 7 - A P I P I N G C R I T E R I A S I V B STAGE NO IRN-CCBD ENTERED P N E U SUP SYS -.. 02-04-66 LOFA 040-347 MSFC-E �. APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE DATE 2 9 J U L 6 6 -- --- -- DOCUYENT NUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD ACTUAL SCHED REL DATE R E L ' D A T E PANEL MO DA Y R MO DA YR CODE 64 --. PREPARING INTERFACE AREAS CENTF9 OR C E I NUMBERS ACT. TY - ENTERED A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 HSFC-K-DT A PHY I C D FWD UMB SWING ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-2 1-66 LO-FA 040-347 NSFC-DT A PHY I C D XU UMB SWING ARM NO 3 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5 - 6 6 LOFA 090-347 MSFC-K-Dl 08-02-65 LO-FA 08-02-65 LO-FA 08-02-65 LO-FA - - - FHY I C D UH5 NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBO NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED (SH C.MASTI1) SH. M A S T I V PHY I C D OBAT T A I L LOX UMB S - I B / I 8 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 4 -- P H Y S I C A L I C D BOAT. T A I L FUEL UHB S - I B / I B �APOLLO I N T E R F A C F CONTRr'!. AS D A T E 2 9 J U L 66 -- --- -- - 207 ----- 3 D G S DOCUMENT N U M B E R , O R R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCSD NUMBER ICD-CCBD IRN-CCBD 010-347 KSC-P PHY I C D BOAT T A I L COND UMBLS S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 08-02-65 LO-FA 010-347 KSG-P A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCED ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 03-02-66 LO-FA 220-347 KSC-P A PHY I C D S - I V B / I U COOLING U N I T / I B NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 01-07-66 LOFA 220-347 USC-P P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 12-30-65 LO-FA 220-347 MSFC- PHY I C D VACUM MONITORING CONSOLE SAT I B ICO-CCBD 2 0 1 - 6 6 - 0 1 4 1 IRN-CCRD 2 0 1 - 6 6 - 0 2 8 5 01-10-66 LO-FA 040-347 - MSFC- - R 1 FWD (SW ARM = 1 ) LO-FA - * - IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ENTERED ENTERED ENTERED ENTERED ENTERED \ I J 651CD5898 PKEPA INTERFACE AREA< CENTE OR C E I NUMBER: ACTIV 08-02-65 NO NO NO NO NO .I 6 5 I C D 5 8 9 7 SCHED ACTUAL REL DATE RE: D l T E PANEL MO DA Y k M O DA Y R CODE 20 1-66-0278 201-66-0278 P H Y I C D UMB CONN S I B / I B :* 301 CONT, C H LOG A PHY I C D I U COOLING U N I T L C 3 4 ALTERNATE' 6 �. APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE D A T E 2 9 JUL 66 - - ' [I S - --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E -------I------------- 61 i - DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE -------- -------- -u---- PREPARING INTERFACE AREAS CENTER OR CEI NUMBERS A C T I V I T Y - --------------- ----. *--- NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 A 651CD6000 A PHY I N T F CONT DWG I U FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-16-65 LO-FA A L C 3 7 S I T E P L A N + G E N L o ARRANGE S / C GSE 08-17-65 LO-FC 230-370 KSC-EDV-2 A L C 3 7 S/C DATA TRANS SYS ( W I D E BAND) NO IRN-CCBD ENTERED 08-25-65 LOFC 230-370 KSC-EDV-2 LC-37 S / C F A C - I N S T - CABLE SYS-PHYSICAL NO TRN-CCBD ENTERED 02-09-66 LOFC 230-370 KSC L C 3 7 AC ELEC PWR S Y S 01-28-65 LOFC 230-370 KSC-F L C 3 7 OPNL T V SYS 03-15-65 LOFC 230-370 KSC-F A L C 3 7 SAT I B S/C TRANSPORT ROUTE 03-15-65 LOFC 230-370 KSC-F - 02-08-66 LOFC 230-370 KSC HAZARD PROOF MON FOR S / C GSE L C - 3 7 10-1 5 - 6 5 LOEL 210-370 KSC-LVO-2 S/C 02-11-66 LOEL 230-370 HSFC-ASTR 09-14-65 LOPG 100-230 KSC-EDV A 651CD6004 - LC 37 HAZARD PROOFING S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - A F A C I L I T Y C A B L I N G LC37FORLEM +ESM NO IRN-CCBD ENTERED - ESE TO DC POWER* ~ ~ ' 3 7 A PIP C R I T + I N T F LOC S/C F L D SYS L C 3 7 8 SS .. �APOLLO I N T E R F A C E CONTROL GOCUMENT L O G DATE 2 9 J U L 66 -- --- -- 1c SCHED H D G S j -9 DOCUMENT NUMBER* O R R E V I S I O N NOTICE - .................... F 651CD6069 A 65ICD6100 R 4 R 5 DOC REV --- ) 1 + R E L DATE RE; DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER -------- --Q--------_---_P--_eY____-_P---------- -0--0--- I N T E R F A C E AREAS C E N T E OR C E I NUMBERS ACTIV ------ --------------- ----- 05-1 6-66 LOPG 230-370 KSC-E - 07-01-65 LOFC 230-370 KSC-F L C 3 7 - S / C S E R V I C E STRUCTURE ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 50 IRN-rCCBD ENTERED NO IRN-CCBD ENTERED 08-17-65 LOFC L C 3 7 PAD B AREA ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 12-06-65 LOFC 230-370 MSFC- FUNCT I N T E R F A C E REQS ECS L C 3 7 0 S/C-GSE 03-19-65 LOPG 100-370 KSC-K FUNCT I N T F REQMTS GHE L C 3 7 0 S / C GSE 05-02-66 LOPG 100-370 KSC-E GSE 05-02-66 LOPG 100-370 KSC-E 02-09-66 LOPG 230-390 -KSC-E 06-17-66 LOFC 230-370 KSC-E 09-16-65 LOFA 230-370 KSC-El 8 - L C 3 7 LAUNCH CONTROL CENTER NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - S/C C 65ICD6469 - F 65ICD6500 A LC-37 F 65ICD6580 A L C 3 7 B UT P I P C R I T + l N T F LOC S / C A 651CD6466 PREPA A L C 3 7 8 S A T I B SS P I P C R I T LEM F L D SYS - i ACTUAL. FUNCT I N T F REQMTS GN2 L C 3 7 0 S / C ESE/GSE L C 3 9 A S / C GSE FUNC I N T F REQlGOX INTERFACE S/C GSE T O UMB TWR F L D SYS* KSC-E �APOLLO INTERFACE CONTROL DOCUMENT LOG IAOl DATE 29 J U L 6 6 -- D _ 5 '--- PAGE -- DOCUMENT NUMBER* OK R E V I S I O N N O T I C E .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ...................................... NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTIVITY - -------- - - - - - - ------ ------------- ----.------ ENTERED ENTERED ENTERED 3 7 8 PHY I N T F LEM UMB ARM CABLE REQMTS NO IRN-CCBD ENTERED L C 3 7 PAD AREA ESE/GSE-L/V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 230-370 KSC-EDV 02-1 0 - 6 6 LO-FC 220-370 KSC F O R LV ESE 01-25-66 LOEL 220-210 MSFC-ASTR SAT I B L V ESE TO RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 6 08-17-65 LO-EL 220-200 MSFC-ASTR L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 2 1 02-11-66 LO-EL 220-370 (YSFC-ASTR A L V ESE/INSTRUMENTATION S Y S + RECOPDERS 03-14-66 LOEL 220-200 PIS FC-ASTR - 08-09-65 LO-EL 200-240 #SFC-ASTR LOEL 220-340 WSFC-ASTR 07-13-66 LO-EL 220-347 MSFCc-ASTR 09-22-64 LO-FC 230-340 A F A C I L I T Y CABLES LC-37B IRN-CCBD 2 0 1 - 6 6 - 0 2 0 5 - A 65ICD8001 SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE 68 --- - MSFC COUNTCLOCK TO KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 5 1 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 1 L V ESE TO KSC DATA MEASUREMENTS L V ESE T O WATER DELUGE SYS ICD-CCBD 2 0 1 - 6 5 - 0 0 5 2 LC/34/37/39 T I M I N G + COUNTDOWN D I S T 03-01-66 �APOLLO I N T E R F A C E CONYROL DLICUYENT L O $ , AS D A T t 29 J U L 66 -- --- -- C H D G - DOCUMENT NUMBER9 OR R E V I S I O N NOTICE DOC REV 207 ----- CONT. DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... 11-29-65 LOFC FUNCT I N T F REQMTS ECS MC LEM S / C GSE 05-03-65 LOPG A.C. LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD B L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - - I N T E R F A C E AREAS CENTEI OR C E I NUMBERS A C T I V -----. SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED L C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED 100-300 MSC-N, VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 230-300 MSC-FI 230-300 KSC-Dl 230-347 KSC-D A MOCK-UP - PREPAI -------- -------- ------ -------------- POWER RECe + CONN A S/C - ,ACTUAL SCHED R E L DATE R E L DATE >ANEL MO DA YR MO D A YR CODE 23 AFRM 9 T O ACCESS ARM WHT RM L C 3 4 / 3 7 SM ARM E L E C A B L E NO IRN-CCBD ENTERED LC34/37 S-IB L/V+S/C MISA.LIGN. + F L T R BOX XNST FOR SAT IS VEH L V PROTUBERANCES L C 3 4 / 3 7 11-04-65 LOFA 07-01-65 LO-FC 07-01-65 LOVC 05-07-65 LO-PG 501-66-0039 MSFC �r APOLLO INTERFACE CONTROL DOCUMENT LOG AS' D A T t 2 9 J U L 66 -- --- -- 1 ; - DOCUMENTNUMBER, OR R E V I S I O N N O T I C E --------.------------ DOC REV 207 ----- --- ...................................... - - PAGE 70 ,'--- - PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y - ---- ----.. -,---, -,-,--------,-, - 201-66-0127 201-66-0127 IB 02-23-66 LOPG 000-220 KSC-EDV FUNC I N T F F L U I D REQMTS GN2 SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 2 05-25-65 LO-PG 000-220 KSC-K-DT FUNC I N T F F L U I D REQMTS L H 2 SYS SAT ICD-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 2 0 1 - 6 6 - 0 1 2 8 05-24-65 LO-PG 000-22 0 KSC-K-DT A FUNC I N T F F L U I D REQMTS GN2 SYS S A T NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 0 7 IRN-CCBD 2 0 1 - 6 6 - 0 3 3 8 - CONT. SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO D A . YR CODE DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD IAOL 13 .-'. :\c -,-- - FUNC I N T F F L U I D REQMTS L H 2 SYS SAT I B ICD-CCBD 2 0 1 - 6 6 - 0 0 7 3 IRN-CCBD 2 0 1 - 6 6 - 0 0 7 3 05-24-65 LO-PG 000-250 KSC-K-DT FUNC I N T F F L U I D REQMTS LOX SYS SAT I B 05-25-65 LO-PG 000-250 KSC-K-!IT (-- \. �-i -/ APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 2 D A T E 2 9 JUL 6 6 IH c D DOCUMENTNUMBERp G 5 OR R E V I S I O N NOTICE > 1 AS -- --- -- R R f 2 A 65ICD8606 R R 1 , DOC REV - 1 2 3 J 65ICD8701 - A 80W90207 - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D A YR CODE -------- ----...--- ...----- PKEPd I N T E R F A C E AREAS CENT€ OR C E I NUMBERS A C T I V -------------- ----- 201-66-0130 201-66-0130 201-66-0130 05-25-65 LO-PG 000-250 KSC-K 12-10-65 LO-FA 110-300 KSC-E 01-04-66 LOFA 220-347 HSFC- PHY I C D HAZARDOUS GAS ANALYZER SATURN I B ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA 220-347 HSFC- LOW BAY ESE TO I N S T R U S Y S + REC 02-11-66 LO-EL 220-290 MSFf 02-01-65 FM 000-100 HSFC- FUNC I N T F F L U I D REQMTS RP-1 ICD-CCBD 20 1 - 6 6 - 0 1 3 1 IRN-CCBD 2 0 1 - 6 6 - 0 1 3 1 IRN-CCSD 2 0 1 - 6 6 - 0 1 3 1 SYS SAT PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 PHY I C D C A L I P S C / O ICD-CCBD 1 CONT- DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD IRN-CCBD - 207 ----- IB COVER CONSOLE SAT I 8 501-66-0171 F L I G H T MECHANICS P A N E L I C D �U A T t 2 3 JUL 66 AS -- --- -- U 5 - DOCUMENTNUMBERt OK R E V I S I O N N O T I C E DOC REV 208 ----- DOCUMENT T I T L E OR CCBD NUMBER -. SCHED ACTUAL REL DATE R E L .DATE PANEL MO DA Y R MO DA YR CODE -------- -------- ------ A 16331-63A107350 A 16331-63A107393 ,A 4 0 M 0 5 4 1 7 R EM1 C O M P A T I B I L I T Y D E S I G N C R I T E P T A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 08-17-65 IC B D E S I G N C R I T E R I A FOR SAT I S ONBOARD E 3 ' ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 08-06-65 CS - 03-18-65 12-15-65 ELEC I C D ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 COMP I N T F A SOFTWARE ICD-ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 , - 1, - - 72 --- PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTT"'TY - -;------, , ,,,, , , , , --,,,,,,,--------------------- - PAGE ---- ---- ---------I---- 000-100 MSFC-ASTR 0 0 0 - 1 00 MSFC EI 230-300 MSFC £1 220-250 MSFC-ASTR - COMP INTERFACE LV ESE/PROPELLANT SYSTEMS ICD-CCBQ. 2 0 1 - 6 5 - 0 0 4 7 TRN-CCBD 2 0 1 - 6 6 - 0 0 9 4 L V ESE/LAUMCH EQUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 5 MSFC-ASTR SPACECRAFT GSE TO LAUNCH V E H I C L E G5r MSFC-ASTR - I N S T U N I T TO SPACECRAFT ELEC R E < MSFC-ASTR EDS CHECKOUT SCHEMATICS ?4SFC - DEF SAT l B I U CMD SYS GSE/LC-3 - DEF SAT I B SRSC TEST ENCOD/LC-*"&+LC-37 - DEF SRSC DECODER/LC-34 + LC-37 +LC-? INTF DEF S A T I B SRSC I N D PANEL/LC-34+LC-37 MSFC-ASTR MSFG-ASTR MSFC-ASTR HSFC-ASTR �APOLLO I N T E R F A C E C O N T R r l DijCUMENT i.O[; G A T E 29 JUL 6 6 -- --- -- .: C ; H U r v , --- R AS ., DOCUMENT NUMBEKo OR R E V I S I O N NOTICE DOC REV -------------------- --- +++ A 50M12623 - - 208 ----- Ih ~ i ; CONTe PAGI SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV ------------------------------9_----------- 07-15-66 IC SEE-DWG MSFC-, 03-15-66 M-NF 040-090 MSFC-I 09-14-65 LOPG 100-230 KSC-El GSE 0 9 - 1 5-65 LOPG FUNC l N T F REQMTS GN2 L C 3 4 S / C GSE NO IRN-CCBD ENTERED 09-1 5 - 6 5 LOPG FUNC I N T F REQHTS GOX L C 3 4 S / C 09-15-65 LOPG 04-05-66 LOFC 11-10-65 LO-FA 11-10-65 LO-FA DEF SAT I B SRSC CODE PLUG/DECODER I C D SATURN I B / V CONTROL R A T E GYRO PKG P I P C R I T + I N T F LOC S/C NO IRN-CCBD ENTERED F L D SYS L C 3 4 SS FUNC I N T F REQMTS GHE L C 3 4 S / C A L C - 3 4 I N T E R F A C E S / C GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD INTF GSE TO UMB THR CRXT + I N T F LOC S / C F L D S Y S ENTERED ENTERED ENTERED A PHY ICD APS MODULES ON L A U V E H / S A T ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A P I P I N G CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1-66-0305 APS PNEU IB UNITS/IB MSFC-I �D A T E 2 9 J U L 66 AS -- --- -- D S DOCUMENT NUMBER, OR R E V I S I O N N O T l C E _ .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ IRN-CCBD IRN-CCBD 3 65ICD58138 R 3 R 4 R 5 208 ----- PAGE CONT, SCHED ACTUAL R E L D A T E R E L D'ATE PANEL MO D A Y R M O D A Y R CODE -------- -------- ------ 74 --- PREPARING LNTERFACE AREAS CENTEP OR C E I NUMBERS ACTI\ Y' - - - - P I - - - - - - - - - ---------- 201-66-0235 201-66-0281 i A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-2 1-66 LOFA F1S FC-K-DT A PHY I C D FHD UMB SWING ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED .IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA MSFC-DT A PHY i C D I U U h B SWING ARM NO 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5-66 LOFA 090-347 MSFC-K-DT 08-02-65 COFA 010-347 KSC-P+VE - ' I PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ( S H C MASTIII PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED SH M A S T I V 1 08-02-65 LO-FA - PHY I C D OBAT T A I L L O X UMB S - I B / T P ICD-CCBD 20 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 4 08-02-65 LO-FA - P H Y S I C A L I C D BOAT T A I L F U E L UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 08-02-65 LO-FA \ 010-347 KSC-P+VE �AS' DATE 2 9 J U L 66 -- --- -- 5 - 208 ----- H J G D --- -S DOCUMENT NUMBER* DR R E V I S I O N N O T I C E DOC REV --- DOCUMENT T I T L E OR CCBD NUMBER R R 1* I 1 2. J 65ICDS895 R R \ ( * 010-347 KSC-I 08-02-65 LO-FA 010-347 KSC-P A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICO-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED ERN-CCBD 2 C 1 - 6 6 - 0 2 8 2 03-02-66 LO-FA 220-347 KSC-P A PHY I C D S - I V B / I U COOLING U N I T / I B NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 01-07-66 LOFA 220-347 KSC-P 2 3 P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 12-30-65 LO-FA 220-347 MS FC- A PHY I C D I U COOLING U N I T LC34 ALTERNATE NO IRN-CCBD ENTERED IRN-C'CBD 2 0 1 - 6 6 - 0 2 3 3 03-02-66 LOFA 220-347 HSFC- A PHY I N T F CONT DWG IU FLOW CONT VALVE BOX ICD-CCBD 2 0 1-66-0104 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-16-65 LO-FA 290-347 XSC-P. 02-08-66 LOFC 230-370 KSC 1 > J * * " Q \ -------- -------- ------ --------------- ---LO-FA PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD 65ICD5898 R 2 R 3 J , 65ICD5899 R 1 E 651CD6007 . . - CONN S I B / I B FWD (SW ARM ENTERED ENTERED ENTERED ENTERED ENTERED =I) PHY I C D BOAT T A I L COND UMBLS S - I B / I B ICD-CCBD IRN-CCBD J 651CD5894 FFIEP INTERFACE AREAS CENT OR C E I NUMBERS ACTI' 08-02-65 + SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO D A YR CODE ----------------u-- -------------------,----------.----------- - PAI CONT, C 1 I A3' APOLLO INTERFACE CONTROL DOCUMENT LOG :j 201-66-0280 2 0 1-66-0280 LC 37 HAZARD PROOFING S / C �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 29 J U L 66 AS -- --- -- I , DOCUMENTNUMBERI OR R E V I S I O N N O T I C E DOC REV CONT. 651CD6069 , PREPARING I N T E R F A C E AREAS CENTE' OR C E I NUMBERS A C T I V i t Y - F L D S Y S L C 3 7 8 SS A L C 3 7 8 S A T I B SS P I P C R I T LEM F L D SYS L C 3 7 LAUNCH CONTROL CENTER NO IRN-CC$D ENTERED - S/C ESE/GSE 09-14-65 LOPG 100-230 KSC-EDV 05-16-66 LOPG 230-370 KSC-EDV 07-01-65 LOFC 230-370 KSC-F ; 651CD6467 - FUNCT I N T F REQMTS'GHE L C 3 7 8 S / C GSE 05-02-66 LOPG 100-370 KSC-EDV ; 65ICD6468 - FUNCT I N T F REQMTS GN2 L C 3 7 B S / C GSE 05-02-66 LOPG 100-370 KSC-EDV 3 7 8 PHY I N T F LEM UMB ARM C A B L E REQMTS NO IRN-CCBD ENTERED 11-10-65 LOFA . 230-370 KSC-EDV L C 3 7 SS TO L / V ESE/GSE ICD-CCBD 2 0 1 - 6 6 - 0 1 1 3 12-08-65 LO-FC 220-370 KSC-EDV-2 L C 3 7 PAD AREA ESE/GSE-L/V ICD-CCBD 20 1-66-0204 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 02-10-66 LO-FC, 220-370 KSC L C 3 7 PHY I N T F S-1B STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 0 1 0 1 01-10-66 LO-FC 000-370 KSC-EDV 08-17-65 LO-EL 220-200 MSFC-ASTR - - - T ENTERED ENTERED A P I P C R I T + I N T F LOC S / C - ' 76 -- -------- -------- ------ --------------- --------- -------------------- --- ...................................... 65 ICD6068 PAGE SCHED ACTUAL R'EL D A T E R E L D A T E PANEL MO D A YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD NO IRN-CCBD : 208 ----- A F A C I L I T Y CABLES L C - 3 7 8 I RN-CCBD 20 1 - 6 6 - 0 2 0 5 FOR L V ESE - - S A T I B L V E S E T O RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 JUL 66 AS -- --- -- ) ) C H G , DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV 208 ----- CONTo DOCUMENT T I T L E OR CCBD NUMBER --- - -------------------- --- ....................................... IRN-CCBD - '- - - -------- ------- ------ --------------- -----. L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 2 1 SYS + RECORDERS MSFC COUNTCLOCK T O KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 5 1 1 RN-CCBD 201-66-0071 LV ESE TO K S C DATA MEASUREMENTS 02-1 1-66 LO-EL 220-370 MSFC-4 03-14-66 LOEL 220-200 MSFC-I 08-09-65 LO-EL 200-240 MS FC-i LOEC 220-340 MS FC-I '07-13-66 LO-EL 220-347 MSFC-i 03-01-66 LV E-SE TO WATER DELUGE SYS ICD-CCBD 2 0 1 - 6 5 - 0 0 5 2 LC/34/37/39 T I M I N G + COUNTDOWN D I S T 09-22-64 LO-FC 230-340 LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED 10-01-64 LOFA 230-340 MSC-F( 03-07-66 LOFA 230-340 KSC-EI L C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED 11-1 7-64 L O F A 100-300 HSC-NI VERT STOP FOR' LES ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 11-18-64 230-300 8 LC37/39 - PREPAl I N T E R F A C E AREAS C E N T € ; OR C E I NUMBERS ACTIV 201-66-0096 A L V ESE/INSTRUMENTATION - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE LEM SWG ARM UMB D I S C A 1 4 - 1 7 2 C / M ACCESS ARM ADPT' HOOD TO S / C I N T F REOW LOFA 100-300 - MSC-FC HSC-EC �. APOLLO INTERFACE, CONTROL DOCUMENT LOG - DATE 2 9 JUL 66 -- --- -- D S DOCUMt!NT NUMBER, OR R E V I S I O N N O T I C E PAGE DOC REV DOCUMENT T I T L E OR CCBD NUMBER A 65ICD8400 - LC34/37 J 651CD8401 - S-IB F 651CD8700 - J 65ICD8701 J 65ICD8702 R R - 1 2 A 80M90205 - L/V+S/C MISALIGN. SCHED ACTUAL REL DATE R E L DATE PANEL HO DA YR MU O A YR CODE LV PROTUBERANCES L C 3 4 / 3 7 COVER PHY I C D CALOPS CHECKOUT CONSOLE/SAT-IS PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTf' 'Y - -------- -------- ------ --------------- ---------- FOR SAT I B VEH PHY I N T F RETRACTION MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 78. --- 07-01-65 LO-FC 07-01-65 LOVC 12-10-65 LO-FA 110-300 KSC-EDV LOFA 220-347 MSFC-EDV 12-01-65 200-347 501-66-0039 MSFC-P+VE MSFC PHY I C D HAZARDOUS GAS ANALYZER SATURN I S ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCSD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA 220-347 MSFC-EDV LOW BAY ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 MS FC F L I G H T MECHANICS PANEL I C D �) IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG ) -- --- -- C H .G I PAGE D A T E 2 9 JUL 6 6 ) --- 0 " DOCUMENT NUMBER9 OR R E V I S I O N NOTICE .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD A 13M65000 1 6 3 3 1 - 6 3 A 107350 A 16331-63A107393 - R - - 201-66-0114 08-06-65 CS 000-100 MSFC 03-18-65 EI 230-300 US FC 08-12-65 €1 300-100 MSC L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 " IRN-CCBD '20 1-66-0094 12-15-65 EI 220-250 USFC-A L V ESE/LAUNCH EQUIPMENT ICD-CCBD 201-65-0048 I RN-CCBD 2 0 1 - 6 6 - 0 0 9 5 12-16-65 €1 220-2 10 MS FC-A 220-230 MSFC-A E L E C I C D ACE S / C - L / V ICD-CCBD 50 1 - 6 6 - 0 0 8 5 COMP I N T F A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - - 1 - PREPAF I N T E R F A C E AREAS CENTEF OR C E I NUMBERS ACTIVl -------- -------- ------ --------------- ------ B D E S I G N C R I T E R I A FOR SAT I B ONBOARD EDS ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 4 A 40M05417 SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE COMP I N T E R F A C E , . - SPACECRAFT GSE T O LAUNCH V E H I C L E GSE - I N S T U N I T T O SPACECRAFT ELEC REQ MSFC-A - EDS CHECKOUT S C H E M A T I C S MSFC - DEF SAT I B I U CMD SYS G S E / L C - 3 4 + L C - 3 7 ..MS FC-A: - DEF SAT I B SRSC T E S T ENCOD/LC-34+LC-37 DEF SRSC DECODER/LC-34 + LC-37 INTF D E F S A T I B SRSC I N D P A N E L / L C - 3 4 + t C - 3 7 02-1 5 - 6 7 EI 07-1 5-66 MSFC-A! 07-1 5 - 6 6 HSFC-A! 07-1 5 - 6 6 HSFC-A! �APOLLO INTERFACE'CONTROL DOCUMENT LOG DATE 29 J U L 6 6 -- D S --- PAGE -- DOCUMCNT NUMBER* OR R E V I S I O N N O T I C E DOC REV SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO D A YR CODE DOCUMENT T I T L E OR CC8D NUMBER 80 --- PREPARING INTERFACE AREAS CENTFn OR C E I NUMBERS ACTI'. Y - -- A 50M12625 - DEF SAT I 8 SRSC CODE PLUG/DECODER A 50K36801 - I C D SATURN I B / V CONTROL RATE GYRO P U G F 65ICOSOb8 R 7 A 65ICD5368 - P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED INTF F L D SYS L C 3 4 SS 07-1 5 - 6 6 IC SEE-DUG MSFC-ASTR 03-1 5 - 6 6 M- NF 040-090 MSFC-#-ED 09-14-65 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GHE L C 3 4 S/C GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV FUNC I N T F REQPITS GN2 L C 3 4 S/C NO IRN-CCBD ENTERED GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GOX L C 3 4 S / C GSE LOPG 100-230 KSC-EDV LOFC 230-340 K5C-EDV 230-340 KSC-EDV 040-347 HSFC-EDV A LC-34 I N T E R F A C E S / C GSE TO UP16 .TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CRIT + INTF ENTERED ENTERED ENTERED LOC S / C F L D SYS - .*. A PHY I C D APS MODULES ON LAU VEH/SAT ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A PIPING CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 . IB APS PNEU U N I T S / I B 11-10-65 LO-FA 11-10 - 6 5 LO-FA 040-347 HS FC-EDV �) APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 ) ) D A T E 2 9 J U L 66 -- --- -- C H D - DOCUMENT NUMBER? OK R E V I S I O N N O T I C E G --- .................... AS. DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ...................................... IRN-CCBD IRN-CCBD J 65ICD5885 R 2 , 2 0 9 -COhJT, PAG. ----- SCHED ACTUAL REL D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE PREPAI I N T E R F A C E AREAS CENTEI OR C E I NUMBERS ACTIV: -------- -------- ------ --------------- 0----- 201-66-0235 201-66-0281 A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 MSFC-)I A PHY I C D FWD UMB S W I N G ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA 040-347 MSFC-I 08-02-65 LO-FA 010-347 KSC-P+ PHY I C D OBAT T A I L LOX UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 4 - 08-02-65 LO-FA 010-347 P H Y S I C A L I C D BOAT T A I L F U E L UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 08-02-65 LO-FA 010-347 A PHY I C D I U UMB SWING ARM NO 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 - - PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED (SH C MAST111 SH M A S T I V KSC-P+ . KSC-P+ �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 6 6 PAGE -- --- -- D 5 DOCUMENT NUMBER, OR R E V I S I O N N O T I C E J 6SICD5892 R 1 R 2 R 3A . R R DOC REV - 4 5 - DOCUMENT T I T L E OR CCBD NUMBER PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED SCHED ACTUAL REL DATE R E L DATE PANEL HO DA YR MO DA YR CODE PREPAR TNG INTERFACE AREAS CENT!! OR C E I NUMBERS A C T I V I T Y - .( -------- ------- ------ --------------- ----------i 08-02-65 FWD (SW ARM = 1 ) LO-FA 010-347 KSC-P+VE ( 08-02-65 LO-FA 03-02-66 LO-FA P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 12-30-65 LO-FA A PHY I C D XU COOLING U N I T L C 3 4 ALTERNATE NO IRN-CCBD ENTERED IRN-GCBD 2 0 1 - 6 6 - 0 2 3 3 03-02-66 LOFA PHY I C D BOAT T A I L COND UMBLS S - X B / I B ICD-CCBD IRN-CCBD 82, --- 201-66-0280 201-66-0280 A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 20 1 - 6 6 - 0 2 8 2 A PHY I C D S - I V B / I U COOLING U N I T / I B NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - A PHY I N T F CONT DWG I U FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 .! 6 5 I C D 6 0 0 7 - LC 37 HAZARD PROOFING S / C MSFC-K-DT I ' 12-16-65 LO-FA 02-08-66 LOFC �1 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS DATE 2 9 JUL 6 6 -- --- - > cH G D DOCUMENTNUMBERp OR R E V I S I O N NOTICE DOC REV 209 ----- DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD NO IRN-CCBD F L D SYS L C 3 7 8 SS LOPG 05-16-66 LOPG FUNCT I N T F REQMTS GHE L C 3 7 8 S / C GSE 05-02-66 LOPG FUNCT I N T F REQMTS GN2 L C 3 7 8 S / C GSE 05-02-66 LOPG 378 PHY I N T F L E M UMB ARM C A B L E REQMTS 11-10-65 LOFA 02-1 0-66 LO-FC SAT 1 8 LV E S E T O RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 6 08-1 7-65 LO-EL L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 2 1 0 2 - 1 1-66 LO-EL 220-370 MSFC-I 08-09-65 LO-EL 200-240 MSFC-I NO IRN-CCBD ENTERED L C 3 7 PAD AREA E S E / G S E - L / V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 A F A C I L I T Y CABLES L C - 3 7 B IRN-CCBD 2 0 1 - 6 6 - 0 2 0 5 - A L V ESE/INSTRUMENTATION - PREPAI I N T E R F A C E AREAS CENTEI OR C E I NUMBERS ACTIV. 09-14-65 A L C 3 7 0 S A T I B SS P I P C R I T LEM F L D SYS - ACTUAL SCHED R E L DATE R E L DATE PANEL MO DA YR MO D A YR CODE ENTERED ENTERED A P I P C R I T + I N T F LOC S / C - PAGI CONT. KSC FOR L V ESE SYS + RECORDERS MSFC COUNTCLOCK T O K S C T I M I N G ICD-CCBO 2 0 1 - 6 5 - 0 0 5 ' 1 . �A5 30'3 ----- CUNT , ,,- i.1 I s I-, .:I. NT N U M H F R . . / I ;ION N O T I C E DOL REV - . . I " 4 L -; a I !),\I. SCHED REL UATE ! ' A i'i: i)/r.~l;;L MO DA YR klfl Y1Z CODE I l Y CCHO NUPSER o r, . ' 7 Pii; 1NTEC.f:I ' * , ~ F . ?.REAS I ,'1.,'" u i OR CF! NIJYfiERS ACTIVITY i d - ' -_-------------- --.---- 03-01-66 LOEL 220-340 HSFC-ASTR 07-13-66 LO-EL 220-347 MSFC-ASTR l.i/3'c/.~S'I/:i? TI WI!VG + COUNTOOWN D I S T 09-22-64 LO-FC 230-340 * 1.L -.,:,-+/'37/:?C;' S Y .CI:r!r.; C.RM IJWB !.)ISC * A 1 4 0 1 9 Pj1-1 1 f?, !\[-!''C ~ , E I ty hj'r i i.! f+ p,lt3 :.<..:I-L :j<) !\I-<:I .ti![) 10-0 1-64 L0F:I LV ESE T O KSC DATA MEASUREHENTS ' L V ESE TO WATER DELUGE S Y S -------------- ---------- ICD-CCBD 20 1-65-0052 - ' 230-340 . . KSC-EDV 1-'14/37 L/V-F~/': klTCALIGN, FOR S A T TB VEH 07-01-65 LO-FC 700-347 MSFC S-I 8 LV PROTUBERANCES L C 3 4 1 3 7 PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCSD 5 0 1 - 6 6 - 0 1 6 4 COVER PHY I C D CALOPS CHECKOUT CONSOLE/SAT-IB 12-1 0-65 LO-FA 110-300 - KSC-EOV ' �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT L O G . ) -- --- -- - C H / PAGE D A T E . 2 9 J U L 66 9 DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV G DOCUMENT T I T L E OR CCBD NUMBER --- -------------------- --- ........................................ - J 65ICD8702 * * R R 1 2 I A 65IC09240 - A 80M90209 - SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE PREPAP I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVI PHY I C D HAZARDOUS GAS ANALYZER SATURN I S ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 12-10-65 LO-FA 220-347 MSFC-E LOH BAY ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 0 2 - 1 1-66 LO-EL 220-290 MS FC FM 000-100 MSFC-A F L I G H T MECHANICS PANEL I C D 09-09-99 �APOLLO INTERFACE' CONTROL DOCUMENT LOG DATE 29 J U L 6 6 PAGE -- --- -- D S DOCUMENT NUMBER* OR R E V l S I O N N O T I C E DOC REV SCHED ACTUAL REL DATE REL D A T E PANEL MO D A YR MO D A YR CODE -------- -------- DOCUMENT T I T L E OR CCBD NUMBER 1 IAOl -a_--- --86( PREPARING INTERFACE AREAS CENTFQ OR C E I NUMBERS ACT1 Y - ------------- -------- I A 13M65000 A 16331-63A107350 EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 B D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 - ELEC I C D ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 I B ONBOARD EDS COMP I N T F A SOFTWARE ICD-ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 A 40M05466 - LV NO NO NO NO NO NO NO IC 000-100 WSFC-ASTR 08-06-65 CS 000-100 MSFC 03-18-65 EI 230-300 MSFC COMP INTERFACE A L V ESE TO PROPELLANT SYS AND ECS IRN-CCBD 201-66-0179 - 08-17-65 P NSFC- ESE TO LAUNCH EQUIPMENT IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCSD ENTERED L V ESE/PROPELLANT SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 12-15-65 EI L V ESE/LAUNCH EQUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 12-16-65 EX . SPACECRAFT GSE TO LAUNCH V E H I C L E GSE LAUNCH VEH GSE/PROPELLANTS + GASSES GSE . . r .8 220-250 WSFC-ASTR 220-2 10 HSFC-ASTR �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT L O G PAGE SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE # f > D DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT A 40M05468 - LAUNCH V E H I C L E GSE TO LAUNCH E Q U I P GSE 05-15-67 EI 210-220 MSFC-AS 40M37514 - I N S T UN.IT T O SPACECRAFT ELEC REQ 09-0 1-66 EI 000-100 MSFC-AS - EDS CHECKOUT SCHEMATICS 11-30-67 EI 000-220 MSFC DEF SAT 1 8 I U CMD S Y S G S E / L C - 3 4 + L C - 3 7 07-15-66 IC 280-290 MSFC-AS' DEF SAT I S SRSC T E S T ENCOD/LC-34+LC-37 07-1 5 - 6 6 IC 280-290 MSFC-AS' 07-1 5 - 6 6 IC 280-290 MSFC-AS1 07-1 5 - 6 6 IC 280-290 MSFC-AS1 07-1 5 - 6 6 IC SEE-DWG MSFC-AS1 03-1 5-66 M-NF 040-090 MSFC-M-E KSC-EDV I A 40M37717 ' - .'. .. - DEF SRSC DECOOERt'LC-34 + LC-37 INTF DEF S A T I B SRSC I N D P A N E L / L C - 3 4 + L C - 3 7 DEF SAT I B SRSC CODE PLUG/DECODER I C D SATURN I B / V INTF CONTROL R A T E GYRO PKG P I P C R I T + 1 N T F LOC S / C NO IRN-CCBD ENTERED F L D SYS L C 3 4 SS 09-14-65 LOPG 100-230 F U N C ' I N T F REQMTS GHE L C 3 4 S / C GSE 09-15-65 LOPG 100-230 FUNC I N T F REQMTS GN2 L C 3 4 S / C NO IRN-CCBD ENTERED GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV FUNC I N T F REQMTS GOX L C 3 4 S / C GSE 09-1 5 - 6 5 LOPG 100-230 KSC-EDV 04-05-66 LOFC 230-340 KSC-EDV A LC-34 I N T E R F A C E S / C GSE TO UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED . KSC-EDV �APOLLO INTERFACE' CONTROL DOCUMENT LOG IAOl -- --- -- DATE 2 9 J U L 66 D S DOCUMZNT NUMBER, OR R E V I S I O N N O T I C E PAGE DOC REV SCHED ACTUAL REL DATE REC DATE PANEL MO DA YR MO D A YR CODE --88 PREPARING INTERFACE AREAS CENT' OR C E I NUMBERS ACTIb,iY ------- -------- ------ -------------- ---------- DOCUMENT T I T L E OR CCBD NUMBER 09-15-65 LOFA 230-340 KSC-EDV L V ESE TO F A C I L I T Y C A B L I N G LC-34 ICD-CCBD 2 0 1 - 6 6 - 0 3 4 4 10-06-65 LO-EL 220-340 MSFC-ASTR L V ESE TO RANGE SEQUENCING L C - 3 4 ICD-CCBD 2 0 1 - 6 5 - 0 0 3 6 05-28-65 LO-EL 220-340 MSFC-ASTR L V ESE TO I N S T R SYS + RECORDERS ICD-CCBD 2 0 1 - 6 5 - 0 0 3 8 02-18-66 LO-EL r220-200 RSFC-ASTR MSFC COUNT CLOCK TO KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 06-08-65 LO-EL 200-240 MSFC-ASTR L V ESE TO K S C DATA MEASUREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 4 6 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 6 12-15-65 LO-EL 220-340 PISFC-ASTR ~05-28-65 LO-EL 220-340 FISFC-ASTR 11-10-65 LO-FA 040-347 IUISFC-ED!! L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD LV NO NO NO C R I T 4 I N T F LOC S I C F L D SYS ENTERED ENTERED ENTERED ESE TO F A C I L I T Y AC POWER L C - 3 4 IRN-CCBD ENTERED TRN-CCBD ENTERED IRN-CCED ENTERED -. L V ESE TO WATER DELUGE SYSTEM ICD-CCBD 2 0 1 - 6 5 - 0 0 4 0 IRN-CCBD 2 0 1 - 6 5 - 0 0 4 0 PHY I C D APS MODULES ON L A U VEH/SAT IS ....-. ( ;, (\ !' ' �APOLLO INTERFACE CONTROL DOCUMENT LOG 3 DATE 2 9 J U L 66 H D DOCUMENTNUMBEKp OR R E V I S I O N N O T I C E I S --.................... 3 DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ ICD-CCBD IRN-CCBD IRN-CCBD ,, SCHED ACTUAL REL DATE REL D A T E ' P A N E L MO DA YR MO DA YR CODE -------- -we----- PREP INTERFACE AREAS CENT O R . C E I NUMBERS ACT1 ------ --------------- ---- 201-66-143 201-66-0239 201-66-0234 A PIPING CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 APS PNEU U N I T S / I B 11-1 0 - 6 5 LO-FA 040-347 MSFC A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 0 1 - 2 1-66 LOFA 040-347 MSFC A PHY I C D FWD UM8 SWING ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA 040-347 MSFC A PHY I C D I U U M B S W I N G ARM NO 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5 - 6 6 LOFA 090-347 MSFC 08-02-65 LOFA 010-347 08-02-65 LO-FA 08-02-65 LO-FA - - PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED PHY I C D UM8 NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - 1 6 / 1 0 ENTERED ENTERED ENTERED ENTERED (SH C M A S T I I ) SH H A S T I V - KSC- . PHY I C D 0BAT T A I L LOX UMB S - I B / I B .. , . 010-347 . KSC-C �( IAOl PAGE DATE 2 9 J U L 66 -- --- -- D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD - - ------- -------- ------ PREPARING ( INTERFACE AREAS CENTFn OR C E I NUMBERS A C T I , . Y - --------- ( I------ 201-66-0284 201-66-0284 P H Y S I C A L I C D BOAT T A I L FUEL UMB S - I B I I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO ISN-CCBD NO IKN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED FWD (SW ARM = I ) 08-02-65 LO-FA 010-347 KSC-P+VE I 08-02-65 LO-FA 010-347 KSC-P+VE 08-02-65 LO-FA 010-347 RSC-P+VE 03-02-66 LO-FA 220-347 KSC-P+VE 12-30-65 LO-FA 220-347 HS FC-K-DT I I PHY ICD BOAT T A ~ LCOND UHBLS S-IBIB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 J 65ICD5895 R 2 ?I 3 SCHED ACTUAL REL DATE R E L DATE PANEL HO DA YR MO DA YR CODE --90( - 7 A PHY I C D S - I V B I I U COOLING U N I T / I B NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 A PHY I C D I U COOLING U N I T L C 3 4 ALTERNATE ( 03-02-66 LOFA 220-347 HSFC-X-DT I �APOLLO INTERFACE CONTROL DOCUMENT LOG 3 3' -- --- -- DATE 29 JUL 6 6 c H D DOCUMENT NUMBER, OR R E V I S I O N NOTICE DOC REV 3 - - -S -------------------- --- DOCUMENT T I T L E OR CCBD NUMBER ---------------------em----------------- ACTUAL SCHED REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE -------- -------- ------ PREl INTERFACE AREAS CENl OR C E I NUMBERS ACTi ---- ---I------- NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 * 3 * 3 3 1 I ' ' ' ? 3 65ICD5899 R E t 1 65ICD6007 R 1 R 2 A PHY I N T F CONT DWG I U FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-1 6-65 LO-FA 290-341 KSC- - 02-08-66 LOFC 230-370 KSC 09-14-65 LOPG 100-230 KSC- 05-16-66 LOPG 230-370 KSC- FUNCT I N T F REQMTS GHE L C 3 7 8 S I C GSE 05-02-66 LOPG 100-370 KSC- FUNCT I N T F REQMTS GN2 L C 3 7 8 S / C 05-02-66 LOPG 100-370 KSC- 3 7 8 PHY I N T F LEPI UMB ,ARH CABLE REQMTS NO IRN-CCBD ENTERED 11-10-65 LOFA 230-370 KSC- L C 3 7 SS TO L / V ESE/GSE ICD-CCBD 2 0 1 - 6 6 - 0 1 1 3 12-08-65 LO-FC 220-370 K S C- L C 3 7 PAD AREA ESE/GSE-L/V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1-66-02-04 02-10-66 LO-FC 220-370 L C 3 7 PHY I N T F S - I B STAGE TO HOLDDOWM ARM ICD-CCBD 2 0 1-66-0 10 1 01-1 0 - 6 6 LO-FC 000-370 09-22-64 LO-FC 230-341) LC 37 HAZARD PROOFING S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED + I N T F LOC S / C F L D SYS L C 3 7 B SS F 65 I C D 6 0 6 8 A PIP CRIT 3 F 65ICD6069 A L C 3 7 B S A T I B SS P I P C R I T LEM F L D SYS * C 65ICD6467 - - - GSE , 4 LC/34/37/39 TIMING + COUNTDOWN D I S T - KSC KSC-I �DATE 2 9 J U L 6 6 AS -- --- -- ) DOCUMENT NUMBER, OR R E V I S I O N N O T I C E _ .................... 5 DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... - J 65ICD8301 2 1 0 COMT. ----- LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 8 LC37/39 - PAGE SCHED ACTUAL REL D A T E REL D'ATE PANEL M O DA Y R MO DA YR CODE 92 --( . PREPARING INTERFACE AREAS CENTER ( OR C E I NUMBERS A C T I \ ' f ------- ------ -------------- -------- -La---- ( SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED LEM SWG ARH UMB D I S C A L 4 - 1 7 2 t C 3 4 / 3 7 / 3 9 CMD MOD ACCESS ARM C A B L I N G NO IRN-CCBD ENTERED MSC-NAA VERT STOP FOR LES ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD E N T E R E D t4SC-FO C/M ACCESS ARM ADPT HOOD TO S / C ( ( I N T F REQ 11-04-65 LOFA H I S A L I G N - FOR SAT I B VEH 07-01-65 LO-FC 07-01-65 LOVC 12-10-65 LO-FA 110-300 KSC-EDV PHY I C D HAZARDOUS GAS ANALYZER SATURN I 6 ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 5 - 0 2 7 9 12-10-65 LO-FA 220-347 NSFC-EDV LOW BAY ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 FH 000-100 L C 3 4 1 3 7 L/V+S/C S-I B L V PROTUBERANCES L C 3 4 / 3 7 PHY I N T F RETRACTION MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER MSC-EDV 100-300 .. 200-347 501-66-0039 I ' PHY I C D CALOPS CHECKOUT CONSOLE/SAT-I8 F L I G H T MECHANICS PANEL I C D 09-09-99 : ' MS FC MS FC-AERO I �IA01 APOLLO INTERFACE CONTROL DOCUMENT LOG 1 /u : PAG -- --- -- DATE 2 9 J U L 66 C H G D i - DOCUMENT NUMBER* OK R E V I S I O N N O T I C E SCHED ACTUAL REL DATE REL DATE PANEL HO DA YR MO DA YR CODE DOC REV PREPA INTERFACE AREAS CENTE OR C E I NUMBERS A C T I V DOCUMENT T I T L E OR CCBD NUMBER --- ~~~-~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ -------- -------- ------ -------------- ----- .i , , -,,---,------------- -i - A 13/460004 A 13M65000 1 A 16331-63A 1 0 7 3 5 0 , 1. - - 40Ft37515 +++ A 5 0 M 1 2 6 1 3 IC 000-100 MSFC- 08-06-65 CS 000-100 MSFC 03-18-65 €1 230-300 MSFC 08-12-65 EI 300-100 MSC L V ESE/PROPELLANT SYSTEMS ICD-CCBD 2 0 1 - 6 5 - 0 0 4 7 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 4 12-15-65 Ef 220-250 MS FC- L V ESE/LAUNCH EQUIPMENT ICD-CCBD 2 0 1 - 6 5 - 0 0 4 8 IRN-CCBD 2 0 1 - 6 6 - 0 0 9 5 12-16-65 EI 220-210 MSFC- EI 220-230 MSFC- EI 220-250 MS FC- LAUNCH VEH GSE TO ENVIRONMENTAL CONT GSE EI 210-220 HS FC- LAUNCH V E H I C L E GSE TO LAUNCH E Q U I P GSE EI 210-220 LAUNCH V E H I C L E GSE TO F A C I L I T Y GSE EI 210-220 US FC-4 I N S T U N I T T O SPACECRAFT ELEC REQ EI 000-100 MS FC-4 DEF SAT I S I U CMD SYS GSE/LC-34+LC-37 IC 280-290 .HSFC-I ELEC I C D ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 I B ONBOARD EDS COMP I N T F A SOFTWARE ICD-ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - 40M05476 08-17-65 8 D E S I G N C R I T E R I A FOR SAT ICD-CCBD 2 0 1 - 6 6 - 0 0 5 1 i A 16331-63A107393 E M 1 COMPATI B I t l T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 - COMP INTERFACE SPACECRAFT GSE TO LAUNCH V E H I C L E GSE LAUNCH VEH GSE/PROPELLANTS + GASSES GSE . .. MS FC- �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE DATE 29 J U L 66 -- --- -- DOCUMENT NUMBER, OR R E V I S I O N N O T I C E .................... 5OM12614 REV DOCUMENT T I T L E OR CCBD NUMBER --....................................... - 50M12623 - DEF SAT I B SRSC CODE PLUG/DECODER SOH36801 - I C D SATURN I B / V 6 5 ICD5368 , 65ICD5370 - - 07-1 5 - 6 6 IC 280-290 c c C HSFC-ASTR ,- 50M12622 - PREPARING I N T E R F A C E AREAS CENTER OR CEI NUMBERS A C T I V I . -------- -------- ------ --------------- --------- DEF SAT I B SRSC T E S T ENCOD/LC-34+LC-37 - 50M12621 ACTUAL SCHED R E L D A T E R E L DATE PANEL M 0 DA Y R HO DA YR CODE DOC 94 --- - DEF SRSC DECODER/LC-34 + LC-37 INTF DEF S A T I B SRSC I N 0 P A N E L / L C - 3 4 + L C - 3 7 INTF CONTROL R A T E GYRO PKG P I P C P I T + I N T F LOC S / C NO IRN-CCBD ENTERED F L D SYS L C 3 4 SS FUNC I N T F REQMTS GHE L C 3 4 S / C GSE FUNC I N T F REQMTS GN2 L C 3 4 S / C G S E NO IRN-CCBD ENTERED FUNC I N T F REQMTS GOX L C 3 4 S / C GSE A L C - 3 4 I N T E R F A C E S / C GSE T O UMB TWR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD C R I T + I N T F LOC S I C F L D SYS ENTERED ENTERED ENTERED -'WSFC COUNT CLOCK T O KSC TIt4ING ICD-CCBD 201-65-0039 07-1 5 - 6 6 IC 280-290 07-15-66 IC 280-290 WSFC-ASTR 07-1 5 - 6 6 IC SEE-DWG WSFC-ASTR 03-1 5-66 M- NF 040-090 WSFC-M-ED 09-1 4-65 LOPG 100-230 KSC-EDV 09-15-65 LOPG 09-1 5 - 6 5 LOPG 09-15-65 LOPG KSC-EDV 04-05-66 LOFC KSC-EDY 09-1 5 - 6 5 LOFA KSC-EDV 230-340 KSC-EDV -C �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 2 j AS. --- -- DATE 29 J U L 66 H ' G D S -- DOCUMENTNUMBERI OR R E V I S I O N NOTICE 211. ----- CONT. SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D A YR CODE DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- - -------------------- --- ........................................ PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV -------- -------- ------ ------------- ----- 11-10-65 LO-FA 040-347 MSFC- 11-10-65 LO-FA 040-347 MSFC- A PHY I C D AFT UMB SWING ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 MSFC- A PHY I C D FWD UMB SWING ARM NO 3 S - I V B ICD-CCBD 201-66-0290 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA 040-347 MSFC- A PHY I C D IU UMB SWING ARM NO 3 I RN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5 - 6 6 LOFA 090-347 MSFC- - 08-02-65 LOFA 010-347 08-02-65 LO-FA 010-347 A PHY I C D APS MODULES ON L A U VEH/SAT ICD-CCBD 2 0 1 - 6 6 - 1 4 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 9 I RN-CCBD 2 0 1 - 6 6 - 0 2 3 4 A P I P I N G CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 5 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 1 - IB APS PNEU U N I T S / I B PWY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED PHY I C D UHB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED (SH C MASTXI) SH HASTXV . ' KSC-P - KSC-P �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 6 6 -- --- -- O S DOCUMENT NUMBER* OK R E V I S I O N NOTICE AS DOC REV 211 IAOl CON?. DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTIJA L REL DATE R E L DATE PANEL #O DA YR MU DA YR CODE PREPARING INTERFACE AREAS CENT OR C E I NUMBERS ACT:+ s T Y - - -- - PHY I C D OBAT T A I L LOX UM8 S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 4 08-02-65 LO-FA P H Y S I C A L I C D BOAT T A I L FUEL UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 08-02-65 LO-FA 08-02-65 LO-FA PHY I C D BOAT T A I L CON0 UMBLS S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 08-02-65 A A PHYS I C D I N S T R U N I T PNEU CONSOLE/IB ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 A PHY I C D S - I V B / I U COOLING U N I T / I B NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - - 010-347 KSC-P+VE LO-FA 010-347 KSC-P+VE 03-02-66 LO-FA 220-347 KSC-P+VE 01-07-66 LOFA 220-347 KSC-P+VE P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 3 8 12-30-65 LO-FA 220-347 HS FC-K-DT. A PHY I C D I U COOLING U N I T L C 3 4 ALTERNATE 03-02-66 LOFA 220-347 HSFC-K-DT - - - - PHY I C D UHB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED FWD [SW ARM = I ) �i A01 APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE DATE 2.9 J U L 6 6 -- --- -- C H G 3 , LII Y DOCUHENTNUMBERp OR R E V I S I O N NOTICE . . . - I I P I - - - I I " I - - - - - - - DOC REV 1m- DOCUMENT T I T L E OR CCBD NUMBER ........................................ PREPAF INTERFACE AREAS CENTEF OR C E I NUMBERS ACTIVI SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR HO D A Y R CODE -------- ----..,.--- ------ --------------- ------ NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 J 65ICD5899 R 1 A PHY I N T F CONT DWG I U FLOW CONT VALVE BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 F 6SICD6068 12-16-65 LO-FA 290-347 KSC-Pi 02-08-66 LOFC 230-370 KSC 09-14-65 LOPG 100-230 KSC-EC 05-16-66 FOPG 230-370 KSC-EC GSE 05-02-66 LOPG 100-370 KSC-EC FUNCT INTF REQMTS GN2 L C 3 7 8 S / C G S E 05-02-66 LOPG 100-370 KSC-EC 370 PfY i I N T F LEM UMB ARM CABLE REQMTS NO IRN-CCBD ENTERED 11-10-65 LOFA 230-370 KSC-EI L C 3 7 PAD AREA ESE/GSE-L/V ICD-CCBD 2 0 1 - 6 6 - 0 2 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 02-10-66 LO-FC 220-370 KSC 0 1-2 5 - 6 6 LOEL 220-210 MS FC-I 08-17-65 LO-EL 220-200 MSFC-CI LC 37 HAZARD PROOFING S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A P I P C R I T + I N T F LOC S/C F L D SYS L C 3 7 8 SS A L C 3 7 B S A T I B SS P I P C R I T LEM F L D SYS - - FUNCT I N T F REQHTS GHE L C 3 7 B S / C A F A C I L I T Y CABLES LC-37B IRN-CCBD 2 0 1 - 6 6 - 0 2 0 5 - FOR L V ESE SAT I B L V ESE T O RANGE SEQUENCING ICD-CCBD 2 0 1 - 6 5 - 0 0 5 0 IRN-CCBD 2 0 1-66-009b '. , �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 6 6 AS -- --- -- D S DOCUMENTNUMBERv OR R E V I S I O N N O T I C E DOC REV 211 ----- CONT. DOCUMENT T I T L E OR CCBD NUMBER - -------------------- --- ....................................... - L V E S E / 6 0 AC POWER REQUIREMENTS A A 651CD6T05 - A 651CD6770 - - - PREPARING INTERFACE AREAS CENTr OR C E I NUMBERS A C T I V ~ J Y - -------- -------- ------ --------------- -------LO-EL 220-370 MSFC-ASTR L V ESE/ INSTRUMENTAT ION SYS + RECORDERS 03-14-66 LOEL 220-200 ;JISFC-ASTR MSFC COUNTCLOCK TO KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 5 1 IRN-CCSD 2 0 1 - 6 6 - 0 0 7 1 08-09-65 LO-EL 200-240 BfSFC-ASTR LOEL 220-340 HSFC-ASTR 07-13-66 LO-EL 220-347 WSFC-ASTR 230-340 KSC-EDV L C 3 4 / 3 7 / 3 9 CHD MOD ACCESS ARH C A B L I N G NO IRN-CCBD ENTERED 100-300 HSC-I VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 230-300 HSC-FO 201-66-0121 L V ESE TO KSC DATA MEASUREMENTS L V ESE TO WATER DELUGE SYS ICD-CCBD 2 0 1 - 6 5 - 0 0 5 2 tC/34/37/39 T I M I N G + COUNTDOWN D I S T 09-22-64 LO-FC LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD SM SWG ARM UM8 D I S C A 1 4 0 1 9 ENTERED ENTERED 10-01-64 LOFA B LC37/39 - SCHED ACTUAL REL DATE R E L DATE PANEL H O D A Y R MO DA YR CODE 98 --- 02-1 1-66 ICD-CCBD A 65ICD6703 PAGE LEH SWG ARM UMB D I S C A 1 4 - 1 7 2 C/M ACCESS ARM ADPT HOOD TO S / C L C 3 4 1 3 7 L/V+S/C MISALIGN. - I N T F REQ 11-04-65 LOFA 100-300 WSC-EDV FOR SAT 1 8 VEH 07-01-65 LO-FC 200-347 84SfC-P+VE �I A01 APOLLO I N T E R F A C E C O ~ T R O L DOCUMENT LOG DATE 29 JUL PAG 66 -- --- -- C H D G --. C OOCUMENTNUMBERp OR R E V I S I O N N O T I C E _ .................... J 65IC08401 DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - S - I 8 L V PROTUBERANCES L C 3 4 / 3 7 - PHY I N T F R E T R A C T I O N MECH Q-BALL COVER ICD-CCBD - - PHY I C D HAZARDOUS GAS ANALYZER SATURN I8 ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 201-66-0279 ICD-CCBD -------- ------- -----07-01-65 LOVC 12-10-65 LO-FA PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS A C T I V ------*------a- -----. 501-66-0039 MSFC 501-66-0164 PHY I C D CALOPS CHECKOUT C O N S O L E / S A T - I 8 - LOW B A Y SCHED ACTUAL R E L D A T E R E L DATE P A N E L MD DA YR MO DA YR CODE ESE T O I N S T R U S Y S + REC 501-66-0171 12-01-65 LOFA 12-10-65 LO-FA 02-11-66 LO-EL 220-347 MSFC-I �APOLLO INTERFACE CONTROL DOCUMENT L O G DATE 2 9 J U L 6 6 -- D S --a -- DOCUMENTMUMBER, OR R E V I S l O M N O T I C E PAGE 100( -- DOC REV - DOCUMENT T I T L E OR CCBD NUMBER 16331-63Al07350 A 16331-63A107393 - ELEC I C D ACE S/C-L/V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 - LV NO NO NO NO NO NO NO --------------- --------- I - ( COMP INTERFACE 08-12-65 €1 300-100 HSC t 08-06-65 €1 220-250 NSFC-ASTR E1 220-230 N S FC-ASTR EI 220-250 MSFC-ASTR -. ESE TO LAUNCH EQUIPMENT IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IMN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED SPACECRAFT GSE TO LAUNCH V E H I C L E GSE LAUNCH VEH GSE/PROPELLANTS + GASSES GSE LAUNCH V E H I C L E GSE TO LAUNCH E Q U I P GSE - I N S T U N I T T O SPACECRAFT - ! ONBOARD ED$ A L V ESE TO PROPELLANT SYS AND ECS IRN-CCBD 2 0 1 - 6 6 - 0 1 7 9 - - COMB I N T F A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - --..------------- PREPARING INTERFACE AREAS CENTr OR c ~ Nr U M B E R S ACTT~=# ,i 'r' EMI COMPATIBILITY DESIGN CRITERIA ICD-CCSD 2 0 1 - 6 6 - 0 1 1 4 B D E S I G N C R I T E R I A FOR SAT It3 ICD-CCBD 2 0 9 - 6 6 - 0 0 5 1 A SCHED ACTUAL REL DATE REL DATE P A N E L MD B A YR M O D A vn CODE ELEC REQ DEF SAT 18 IU CMD SYS G$E/bC-34+LC-37 - ( �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl DATE 2 9 J U L 66 -- --- -- 1 D S DOCUMENT NUMBER, DRREVISIONNOTICE PAGE DOC REV ___ _ _-_-____---_----___ ........................................ ; DOCUMENT T I T L E OR CCBD NUMBER _-L A 65ICD7167 - A 65ICD7300 - R 2 R R 4 6 F 65ICD7468 A 65ICD7500 * R R 3 , SA - -------a 05-03-65 L C 3 9 LCC F A C I L I T Y S / C ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 03-0 5 - 6 5 LC39 PI'PING NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD LC39/MSS C R I T + I N T F LOC S / C ENTERED ENTERED . ENTERED ENTERED F L D SYS P I P C R I T + I N T F LOC LEM F L D SYS' PREPAR I , I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T ' -------- ------ --------------- FUNCT I N T F RQHTS ECS L C 3 9 / V A B LEM SC GSE A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - SCHED ACTUAL REL D A T E R E L DATE P A N E L HO DA YR MO DA YR CODE LOPG -------a 230-390 KSC-K-Dl 230-390 KSC-F 01-25-65 LOFC 230-390 KSC-F 09-03-65 LOPG 100-200 KSC -. 12-02-65 LOPG 140-390 01-12-65 LOFC 230-390 KSC-EDV 4 L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD ENTERED ENTERED , KSC-F �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 JUL 66 PAGE 19 -- --- -- D S -- DOCUMENT NUMBER, DR R E V I S I O N N O T I C E -- DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ ----------------I-- A L C 3 9 SAT V VEH STAGE + S / C 0 65ICD7010 MISALIGNMENT SCHED ACTUAL R E L D A T E R E L DATE PANEL MU DA YR MO D A YR CODE PREPARING I N T E R F A C E AREAS CEP, 9 OR C E I NUMBERS ACTig I T Y -------- -------- ------ -------------- --------08-13-65 LOFC 100-390 KSC-EDV-2 04-28-65 LOFC 230-390 KSC-F 03-19-65 LOPG 100-395 KSC-K-D? A LC39 CSM + LEM T O F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NU IRN-CCBD E N ~ ~ K E D NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - A 65ICD7052 S/C GSE TO HAZARD PROOF MON SYSTVLC-39 A L C 3 9 VAB H I G H BAY AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBO ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A 65ICD716.6 ' - FUNCT 1 NTF REQS E C S L C 3 9 V A B a S / C - G S E �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 AS -- --- -- D S DOCUMENT NUMBER, OR R E V I S I O N NOTICE DOC REV - E 651CD7006 * CONT- PAGE 1' -. SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO D A YR CODE PREPARIN) I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY - -------- -------- ------ --------------- DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD - 507 ----- --------I 50 1-66-0083 L V ESEt'PROPELLANT SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 L V E S E TO LAUNCH EQUIPMENT ICD-CC0D 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 SC E S E TO L V E S E 12-01-66 €1 220-230 MSFC-AST' I N S T U N I T T O SPACECRAFT ELECT REQ 11-0 1-66 EI 000-100 MSFC-AST 05-06-67 CS 000-100 MSFC-ASTI EDS CHECKOUT SCHEMATICS 05-30-68 E I 000-220 MSFC I C D SATURN I B / V 03-15-66 M- NF 040-090 MSFC-M-El 01-28-65 LOFC 230-390 KSC-F L C 3 9 DATA TRANS S Y S ( W 1 D E BAND) NO IRN-CCBD ENTERED 02-02-65 LOFC 230-390 KSC-F L C 3 9 CPNL INTERCOM SYS-S/C 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 KSC 03-23-65 LOFC 230-390 KSC-F 03-1 5-65 LOFC 230-390 DES OF SATURN S A - 5 0 7 + APOLLO SC EDS CONTROL R A T E GYRO PKG L C 3 9 S I T E P L A N + G E N L ARRANGE-S/C NO IRN-CCBD ENTERED L C 3 9 FAC GSE ESE/GSE INST C A B L I N G - L O C / R D U T I N G S/C 4 L C 3 9 OPNL T V SYS-FAC-S/C ESEIGSE A L C 3 9 S A T V TRANSP ROUTES - S / C - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 19: OAT€ 29 J U L 6 6 --- -- --- -- D S DOCUMENTNUMBER* OR R E V I S I O N N O T I C E DOC REV - - -------------------- --- - DOCUMENT T I T L E OR CCBD NUMBER ........................................ - -------- -------- ------ PREPESIYG I N T E R F A C E AREAS CEN' OR C E I NUMBERS ACTIVITY - ---------- -------------I- L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 IRN-CCBD 50 1 - 6 6 - 0 1 9 8 L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 B ENVELOPE L E M / S - I V B / I U ICD-CCBD 50 1-66-0099 - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR M U DA YR CODE CLEARANCE P H Y S I C A L - INSTRUMENT U N I T TO SPACECRAFT PHYS REQ NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 6 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT T O Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 PHYS REQ MSFC B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 201-66-0114 B D E S I G N C R I T E R I A FOR SATURN V ONSOARD EDS ICD-CCBD - 000-100 MSFC-ASTR 08-06-65 C-S 000-100 iclSFC- 03-18-65 €1 300-230 MSC 3 0 0 - 1 00 14SC 501-66-0078 E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 A SOFTWARE I C D - A C E COMP I N T F S/C-L/'J COMP I N T E R F A C E �APOLLO INTERFACE CONTROL DOCUMENT LOG ,. . AS DATE 2 9 JUL 6 6 -- D S --- -- DOCUMENT NUMBER, OR R E V I S I O N NOTICE J 65ICD9776 I DOC REV - 65ICD9776-001 k+ 66ICD7009 A 80M90506 CONT. DOCUMENT T I T L E OR CCBD NUMBER PAGE 1 - SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE 02-10-66 P H Y I C D P I P E C R I T S I C FWD UHB SERV UN SV ICD-CCBD PREPARIN INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y - -------- - - - - - - ------ -------------LO-FA 010-220 -I---- MSFC-EDV 501-66-0180 SEE, B A S I C NUMBER FOR R E V I S I O N ~ T I T L E ~ E T C o - 66ICD7007 506 ----- ' SEE-DWG PHY I C D + P I P C R I T HAZ GAS ANALYZER SATV ICD-CCBD 5 0 1 - 6 6 - 0 1 0 0 I RN-CCBD 5 0 1 - 6 6 - 0 3 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 5 02-04-66 LO-FA 220-000 HSFC-EDV A L C 3 9 M L PHY L O C PORT I U WATER ACCUM CART ICD-CCBD 5 0 1 - 6 6 - 0 2 0 7 03-02-66 LO-FA 220-390 KSC-EDV 02-08-66 LOFC 230-390 KSC 01-20-66 LOFC 230-390 KSC-EDV- 10-01-66 FM 000-100 MS FC-AER - - LC-39 HAZARD PROOFING-S/C L C 3 9 S/C DOC- POHER S U P P L I E S F L I G H T MECHANICS PANEL I C D �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG . .- D 5 DATE 2 9 J U L 66 PAGE l C -- --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E -. DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -------------------- --- ....................................... ICD-CCBD IRN-CCBD SCHED ACTUAL R E L D A T E R E L DATE PANEL MO D A YR MO D A YR CODE P R F " 4 R IN( I N T E R F A C E AREAS C E , .R OR C E I NUMBERS ACTIVITY -------- -------- ------ --------------- 501-66-0045 501-66-0327 SEE B A S I C NUMBER FOR R E V I S I O N t T I T L E t ETCo 65 I C 0 9 7 6 6 - 0 0 3 - J 65ICD9769 - - . - SEE-DWG PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 02-1 0-66 LO-FA 220-390 KSC-K-DT PHY I C D S - I C PNEU CONSOLE RKS 1 - 2 - 3 + 4 ICP-CCBD 5 0 1 - 6 5 - 6 1 09-1 5 - 6 5 LO-FA 220-390 KSC-X-Dl PHY I C D PNEU CONSOLES 5 9 6 0 7 + 8 S - I C ICD-CCBD S O 1 - 6 5 - 3 4 08-09-65 LO-FA 220-390 KSC-P+VE PHY I C D S - I C PNEU CHECKOUT RKS 1-2-3+4 ICD-CCBD 501-65-46 09-24-65 LO-FA 220-390 MSFC-ECV PIPING CRITERIA S-IC ICD-CCBD 5 0 1-66-0046 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 220-280 M$$c-P+v~ 12-09-65 LO-FA 210-390 K S r SDV:- P I P C R I T S - I C F L U S H + PURGE U N I T SAT V ICD-CCBD 5 0 2 - 6 6 - 0 0 4 7 - 02-07-66 LO-FA 010-390 MSEC-EDX PHY I C D + P I P E C R I T S I I L E A K DETECT SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 4 IRN-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-10-65 LO-FA 020-220 MSFC-EDV PNEU CONSOLE SET A S - I 1 STAGE GSE PLACEMENT ON MBL LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 50 1-66-0129 J 651CD9773 --------a . r �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 DATE 2 9 JUL 6 6 - -- --- -- O S DOCUMENT NUMBER, OR REVISION NOTICE DOC REV _-- -------------------- --R J 651CD9759 DOCUMENT T I T L E OR CCBD NUMBER ....................................... IRN-CCBD 1 - - - - -u---- PREPARIN I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y - ------ -------------- --I---- -------a 501-66-0292 PHY I C D APS PNEU CONS D S V - 4 B - 4 3 6 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 V P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 PHY I C D S - I C ICD-CCBD - ACTUAL SCHED R E L D A T E R E L DATE P A N E L MO D A YR MO DA YR CODE INERT PREFILL 501-65-47 + PIPING CRIT PHY I C D S - i i PNEU CONSOLES 5 7 - 4 1 B / S A T ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 4 IRN-CCBD 5 0 1 - 4 6 - 0 3 0 1 PHY I C D S I I PNEU CONSOLE 5 7 - 4 l C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 I RN-CCBD 5 0 1 - 6 6 - 0 1 2 8 IRN-CCRD 5 0 1 - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 1 D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCSD 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 V V V V P I P I N G C R I T E R I A S-11 PNEU SYS/SATURN V 06-21-65 LO-FA 220-390 - KSC-P+VE 02-10-66 LOFA 220-390 MSFC-EDV 09-15-65 LO-FA 220-390 MSFC-EDV 06-25-65 L e F A 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 02-11-66 LO-FA 220-390 MSFC-EDV �A P O L L O I N T E R F A C E C O N T R O L DOCUMENT L O G IAOl --- -- D A T E 2 9 J U L 66 -.- O S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E O R C C B D NUMBER ICD-CCBD IRN-CCBD IRN-CCBD J 65ICD9751 R - 1 - - - 501-66-0178 501-66-028 1 501-66-0288 06-1 8-65 LO-FA 040-390 KSC-P+VE UMBILICAL + SERVICE CONNECTIONS I U I C D - C C B D 501-65-35 I R N - C C B D 501-66-0285 1 RN-CCBD 501-66-0284 06-1 8-65 LO-FA 090-390 KSC-P+VE KSC-K-DT PHY I C D S - I V B PNEU CONS DSV-48-432/SAT I CD-CCBD 501-66-0107 V 06-21-65 LO-FA 220-390 PHY I C D S - I V B V 06-21-65 LO-FA ' 220-390 01-2 8-66 LO-FA 020-390 06-21-65 LO-FA 220-390 KSC-P+VE 09-15-65 LO-FA 220-390 MSFCzEDV 09-15-65 LO-FA . 220-390 PNEU CONS DSV-4B-433/SAT 501-66-0105 P I P I N G CRITERIA S-IVB I C D - C C B D 501-66-0043 I RN-CCBD 501-66-0374 PNEU CONS S E T L C 3 9 PHY I C D S-IVB HT EXCH DSV-4B-438/SAT I C D - C C B D 501-66-0106 V P H Y ICD IU C O O L I N G U N I T + P I P I N G C R I T ICD-CCRO I RN-CCBD - PREPARING INTERFACE AREAS CENTE' O R C E I NUMBERS ACTIVL~U UMB + S E R V I C E C O N N E C T I O N S S - I V B , FORWARD I C D - C C B D 501-66-0177 I R N - C C B D 501-66-0283 ICD-CCBD - SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA Y R MO D A YR C O D E KSC-P+VE - KSC-P+VE 501-65-49 50 1-66-0376 PHY TCD I U PNEU CONS + P I P I N G C R I T E R I A I C D - C C B D 50 1-65-48 HSFC-EDV �D A T E 29 J U L 66 D S &'-, D O C U M E N T . NUMBER? O R R E V ~ S ~ O NNO.T I C E ------ - ----- 4----.----- DOC REV --- T I T L E C K C C e c <;ii?~\E;! ----DQCUFENT ,-------&----.^ ----------r- . --,,----- - f RAI-CCBB-'901 - 6 b - 0 2 9 0 IRM-CCBD 5 0 1-66-0296 I R N - C U D 501-66-0373 - P H Y r C D L A U V E H S-I C FWD l l M h / L C 3 3 G S E 08-09-65 LO-FA 910-390 x 5<- 06-28-65 LC-FA i.120-390 : .,. . . : ',.- . - 06-2 1-65 LC-FA 020-39C 1 06-21-65 LO-FA 020-390 - -. 06-28-65 020-390 6.I. - : ... ICC-CCBD 501-h5-37 IRN-CCBD 501-66-0190 IRN-CCBD ~01-bb-03Y4 ENTEKED NO I R N - C G R D - UMB + S t i t V C(jb;!li-LTiTj!iS 5 - 1 1 I:.jTFl;h: 9 .ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBG 501-66-011i IRN-CCBL 5C 1-66-1329 1 I RN-CCBC > C L-66-0Zcj!, IRN-CCBD J 65ICD9748 R 503,-6b-i27ii ' - Ut48ItTCAL + SE1'V C ~ j h \ S I I - U M B I L I f A L + SERV: CONM L O X DISCONNECT - S-El-.LH2 DISC ICD-CCBD 50 1-66-0126. I RN-CCBD 50 1-66-01 2 8 . 1 - U M B I L I C A L + SERVICE CONN S-XI .FORWARD ICD?CO%Q .501?';66fOEZ5 IRN-CCBD 501-66-Q%29 I RN-CCBD 501-&6+Q397 N O IRN-CCBD ENTERED R 2 R.. - 3 R \. ICD-CCBD 501-6: -G i 2 7 I RN-CCB0 501-66-0127 5 - UMB + S E R V C O N N E C T I O N S S-I.V'B AFT LO-FA , �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 191 DATE 2 9 J U L 66 -- --- - O S - DOCUMENT NUMBER, OR R E V I S I O N N O T I C E --...----------------R --- DOC REV DOCUMENT T I T L E OR CCBO NUMBER --- ---_------------------------------------ 1 IRN-CCBD - - LOPG 000-260 KSC-K-DT P I P C R I T APS PROP S E R V I C I N G SAT V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-EDV 08-10-65 LO-FA - 3-4 S I C AFT 501-66-0299 5 0 1-66-0289 501-66-0378 UMB + SERV CONNS P L A T E NO 1-2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT 08-18-65 LO-FA S-IC AFT 08-10-65 LO-FA M O T I O N ENV A F T UMB P L A T E S 1 ~ 2 ~ + S -3 IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-10-65 LO-FA 010-210 KSC-P+VE PHY I C D LAU VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 6 08-09-65 LO-FA 010-390 KSC-P+VE * UMB SERV CONNS P L A T E NO 3-2 ICD-CCBD 5 0 1 - 6 5 - 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 I N T K U M B / L C 3 9 GSE -. -------- -------- ------ --------------- ---------05-19-65 XRN-CCBD IRN-CCBD IRN-CCBD - - FUNCT I N T F F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED AND - PREPARING I N T E R F A C E AREAS C E N T OR C E I NUMBERS ACTIL LTY 501-66-0041 - UMB SERV CONN P L A T E ICD-CCBO 50 1 - 6 5 - 4 0 - SCHEO ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO D A YR CODE �APOLLO INTERFACE CONTROL DOCUMENT LOG AS DATE 29 JUL 6 6 -- --- -- DOCUMENT NUMBER, OR R E V I S I O N NOTICE 506 ----- DOC REV DOCUMENT T I T L E OR CCBD NUMBER IAOl CONT. PAGE 1' -. SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR M O D A YR CODE - - - - ICD-CCBD - - - -- PREPARINl INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y - - - - - - - - -- - - - - 501-66-0082 S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CC8D 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSF€-KSC FUNCT I N T F F L U I D REQMTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRM-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG FUNCT I N T F F L U I D REQMTS LH2 SYS SAT V NO IRN-C'CBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG FUNCT I N T F F L U I D REQMTS L O X SYS SAT V ICD-CCBD 5 0 f - 6 6 - 0 0 4 0 I RN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 ' 66-03-65 LOPG 06-15-65 LOPG FUNCT I N T F F L U I D REQMTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 . . S Y S SAT V - �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 JUL 66 -- --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E AS DOC REV 506 ----- CONT, DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ ICD-CCBD 65ICD9142 . - -- . R - 1 - - - -- SCHED AC'TUAL REL DATE REL DATE PANEL MO DA YR MO DA YR CODE PREP.:RINC I N T E R F A C E AREAS C E h .R OR C E I NUMBERS ACTIVITY - 501-66-0136 WIND LOAD A L L E V I A T I O N SYS F A C I L TO L / V LOFC 000-040 MS FC 03-09-66 LO-EL 220-390 MSFC-ASTP L V ESE TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 08-14-65 LOEL 220-390 MSFC-ASTR L V E S E / 6 0 A C POWER REQUIREMENTS ICD-CCBD 501-66-0174 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 02-1 1-66 LO-EL 220-370 HSFC-ASTR L V ESE T O I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL 220-290 MSFC-ASTR MSFC COUNT CLOCK T O KSC T I M I N G L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED 08-14-65 LOEL 200-390 MSFt ASTR L V ESE TO KSC DATA MEASUREMENTS 02-11-66 LOEL 220-290 MSFC-ASTR LOW BAY ESE T O I N S T R U SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 MSFC 02-11-66 LO-EL 220-290 MSFC-ASTR A F A C I L I T Y C A B L E S FOR LAUNCH V E H I C L E E S E ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 501-66-0123 NO IRN-CCBD ENTERED 651CD9201 PAGE 1f2 4 REC LOW B A Y ESE TO I N S T R SYS AND REC 09-01-66 a �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 - DATE 29 J U L 66 -- --- -- D DOCUMENT NUMBER* OR R E V I S I O N N O T I C E __ _ ___________________ S DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD J 65ICD8302 - - - -------- -------- ------ PREPAR I N I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY - ------- ----------I-- ENTERED ENTERED ENTERED 11-17-64 LOFA 230-340 KSC-DL 03-17-65 LOFA 230-300 KSC-DE I N T F REQ 11-04-65 LOFA 100-300 MSC-EDV COVER 12-10-65 LO-FA 110-300 KSC-EDV SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC 220-390 MSFC L C 3 9 V A S H I G H BAYS TO L / V 11-19-65 LOFC 220-390 LC 39 V A B LOW BAY AREA TO L/V-ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-EDV- L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 G2-14-66 LO-FC 220-390 KSC-EDV- L C - 3 9 PAD AREA L / V ES,E/GSE ICD-CCBD 50 1 4 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EDV- S-IC/.!jL, 04-05-66 LO-FC 220-390 MS F f LC34/37/39 CMD MOD ACCESS ARM C A B L I N G V E R T STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP - SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR HO D A YR CODE C/M 2 3 AFRM 9 T O ACCESS ARM WHT RM ACCESS ARM ADPT HOOD 10 S / C PHY INTF R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 ESE/GSE YQLD DOHN. A..RMS PHYSICA:L REQMTS . KSC-F -. �IAOl APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE 18 DATE 2 9 J U L 6 6 -- --- - DOCUMENT NUMBER, OR R E V I S I O N NOTICE .................... -- DOC REV --- R 16 65ICD7767 R 2 R 3 R 4 R 5 65ICD7788 DOCUMENT T I T L E OR CCBD. NUMBER - - L C 3 9 A ML P I P C R l T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - FL SYS 08-20-65 LOFA 230-390 11-17-64 LOFA 230-390 KSC-DE L C 3 9 PHY I N T F C GOX COND PNL LEAK TS U N I T NO IRN-CCBD ENTERED 07-22-65 LOFA 230-390 KSC-EDV ACCESS ARM + SERV MODULE CABLE REQMTS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 09-22-65 LOFA 230-390 KSC-EDV 09-22-64 LO-FC 230-340 POWER REC- + CONN 11-29-65 LOFC 230-347 KSC-EDV-2 FUNCT XNTF REQMTS ECS MC LEM S / C GSE 05-03-65 LOPG 230-300 KSG-K-DT LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 10-01-64 LOFA 230-340 MSC-FO-HJ 03-07-66 COFA 230-340 CSC-EDV: LC39-LUT GSE CABLES-GAS LC/34/37/39 A S/C - - ENTERED - NO LEM U M B I L I C A L AND T E S T IRN-CCBD ENTERED 6 5 1CD8001 PREPARINC INTERFACE AREAS CE? I? OR CEY NUMBERS ACTiSITY -------- -------- ------ --------------- --------- -------------a_----------------------- NO IRN-CCBD - SCHED ACTUAL REL DATE R E L DATE PANEL MO DA Y R M O O A YR CODE AeC- B LC37/39 N I T SYS . KSC-EDV CABLES FOR L C 39 T I M I N G + COUNTDOUN D I S T SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED LEM SKG- ARM UMB D I S C A L 4 - 1 7 2 - - �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 66 PAGE -- --- - D 5 DOCUMENT NUMBERY DR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUHBER SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO DA YR CODE PREPARIf INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T , - --_---- -----o------- I - - LC39/HSS PIP CRIT + I N T F LOC L E F~L D SYS 12-02-65 LOPG 140-390 KSC-EDV 01-12-65 LOFC 230-390 KSC-F FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO IRN-CCBD ENTEREO 03-19-65 LOPG FUNCT I N T F REQHTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-K-Dl 02-09-66 LOPG 230-390 KSC-EDV 02-1 0-66 L/-FC 230-300 # 5,C 03-19-65 LOPG 100~390 KS C-4-.Ol 11-05-64 LO-FC 230-390 HSC-NAA L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD ENTERED ENTERED L C 3 9 A S / C GSE FUNC I N T F REQrGOX LC-39 PAD B S/C FUMCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE 8 L C 3 9 L U T GSE SYSTEMS AFRM C O N F I G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED . NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED ' NO IRN-CCBD ENTERED NO - 1RN-CCBD ENTERED NO IRN-CCBD ENTERED : - KSC-EOV �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 3 U L 66 -- --- -- D S .- - DOCUMENT NUMBER, OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ....................................... . . . ACTUAL SCHED REL DATE REL DATE PANEL MO DA YR MO D A YR CODE -------- ------- ------ -------------- . NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD ENTERED ENTERED ENTERED - . - FUNCT INTF' REQS - FUNCT I N T F RQMTS ECS L C 3 9 / V A B - ECS ~ ~ V3 A B SIC-GSE 9 L E M S C GSE L C 3 9 . LCC F A C I L I T Y S / C ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD 'ENTERED 03-19-65 LOPG 05-03-65 LOPG 03-05-65 ' . A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD:ENTERED' NO IRN-CCBD ENTERED NO ' I RN-CCBD ENTERED NO IRN-CCBD ENTERED NOs:% WN+Cf;BD~:EM'IERED: NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED . . . -- E 0 3 9 r : P t P f NG C&LT1i*, INTF. L-OC S / C FLD SYS NO; NO NO NO IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ENTERED ENTERED ENTERED ENTERED INTERFACE A R E A L OR C E I NUMBERS 01-25-65 LOFC 09-03-65 LOPG �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 DATE 2 9 J U L 66 -- --- -- 0 - DOCUMENT NUMBER, DR R E V I S I O N N O T I C E DOC REV __ _ __ ____-___-_-_ ____-_ --- ........................................ S I A 65ICD7004 - E 65ICD7006 0 65ICD7010 DOCUMENT T I T L E OR CCBD NUMBER L C 3 9 OPNL T V SYS-FAC-S/C ESE/GSE SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE ------- -------- ------ PREPARIF I N T E R F A C E AREAS C E N T E R OR CET NUMBERS A C T I V I T Y - a s - ------ 03-23-65 LOFC 230-390 KSC-F A L C 3 9 SAT V TRAMSP ROUTES -S/C 03-1 5 - 6 5 LOFC 230-390 KSC-EDV- A L C 3 9 SAT V VEH STAGE 4 S / C M I S A L I G N M E N T 08-13-65 LOFC 100-390 KSC-EDV- 02-08-66 LOEL 230-390 KSC-LVO- 04-28-65 LOFC 230-390 KX-F A L C 3 9 CSM + LEM T O F A C I L I T Y CABLES NO NO NO NO NO NO NO NO NO NO NO NO NO A 6 5 1 ~ ~ 7 0 5 2 - S/C IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED GSE T O HAZARD PROOF MON S Y S T v L C - 3 9 A L C 3 9 VAB H I G H B A Y AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED , NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED Nn T R N - C C R D FNTFRFD �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG P A G E 11 -. 0 DOCUMENTNUMBER* OR R E V I S I O N N O T l C E -- -S .................... DOC REV --- DOCUMENT T I T L E OR CCBD NUMBER 16331-63A 1 0 7 3 9 3 A 4 0 M 0 5 5 1 4 '. 40M37522 5 0 1-66-0085 A SOFTWARE I C D - A C E S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - - PREPAR IM I N T E R F A C E AREAS CE -R OR C E I NUMBERS A C T I V I T Y -------- -------- ------ --------------- -------- -----------------O-----------QO--P---- ICD-CCBD A SCHED ACTUAL R E L D A T E R E L DATE P A N E L MD DA YR MO DA YR CODE COMP I N T E R F A C E 08-12-65 EX 300-100 L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 12-15-65 €1 220-210 MS FC-AST L V ESE TO LAUNCH EQUIPMENT ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 12-09-65 €1 220-210 MSFC-ASTI . MSC SC E S E TO L V . E S E 11-06-66 EI 220-230 MS FC-ASTI I N S T U N I T T O SPACECRAFT ELECT REQ 09-01-66 EI 000-1 0 0 MSFC-ASTI 000-100 MS FC-ASTI DES OF SATURN S A - 5 0 6 ICD-CCBD 5 0 1 - 6 6 - 0 2 7 9 + APOLLO SC-107 EDS 03-11-66 CS ' A 40M37718 - EDS CHECKOUT SCHEMATICS 02-28-68 EI 000-220 MSFC + A 50M36801 - I C D SATURN I B / V 03-15-66 M-NF 040-090 MSFC-M-EI 01-28-65 LOFC 230-390 KSC-F L C 3 9 DATA TRANS SYS ( W I D E BAND) NO IRN-CCBD ENTERED 02-02-65 LOFC 230-390 KSG-F - L C 3 9 OPNL I N T E R C O M SYS-S/C 02-06-65 LOFC 230-390 KSC-F - L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G 02-08-66 LOFC 230-390 KSC - - CONTROL R A T E GYRO PKG L C 3 9 S I T E P L A N + GENL ARRANGE-S/C NO IRN-CCBD ENTERED GSE ESE/GSE SIC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 DATE 2 9 JUL 6 6 - -- --- -- O S DOCUMENTNUMBERl OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER _-- ------------------- --- ........................................ - SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR N O D A YR CODE PREPARIN I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y - -------- -------- ------ -------------- -------- L A U V E H i S P A C E C R A F T PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 8 L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 B ENVELOPE I E M / S - I V B / XU CLEARANCE P H Y S I C A L ICD-CCBD 501-66-0099 - I N S T R U M E N T U N I T TO SPACECRAFT PHYS REQ ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 NO IRN-CCBD - SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRM-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 501-66-0242 PHYS REQ B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 A A 13M60004 13M65001 A 16331-63Al01350 - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 201-66-0114 0 D E S I G N C R I T E R I A FOR SATURN V ONBOARD EDS ICD-CCBD 5 0 1 - 6 6 - 0 0 7 8 - E t E C I C D ACE S / C - L / V COMP I N T F OOOilOO MSFC 000-100 MSFC- AS1 01-28-66 TC 000-100 HSFC-AS7 08-06-65 C-S 000-100 MSFC 300-230 MSC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 JUL 66 P A G E 11 -- --- - .- D S DOCfJMENT NUMBER, OR R E V I S I O N N O T I C E - .................... -. DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - PHY I C D P I P E C R I T S I C FWD UMB SERV ICD-CCBD 65ICD9776-001 * - 661CD1009 + A 80M90505 PREPARINI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT-'!ITY - -------- -------- ------ --------------- --UN SV 02-10-66 LO-FA 010-220 a_--- MSFC-EDV 501-66-0180 SEE-DWG SEE B A S I C NUMBER FOR R E V l S I O N o T I T L E , E T C o PHY I C D + P I P C R I T HAZ GAS ANALYZER SATV ICD-CCBD 5 0 1 - 6 6 - 0 1 0 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 5 02-04-66 LO-FA 220-000 MSFC-EDV A L C 3 9 ML PHY LOC PORT I U WATER ACCUM CART ICD-CCBD 5 0 1 - 6 6 - 0 2 0 7 03-02-66 LO-FA 220-300 KSC-EDV 02-08-66 LOFC 230-390 KSC 01-20-66 LOFC 230-390 KSC-EDV-; 07-0 1-66 FM + SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D A YR CODE - LC-39 H A Z A R D PROOFING-S/C L C 3 9 S/C D.C. POWER S U P P L I E S F L I G H T MECHANICS P A N E L I C D �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl D A T t 29 J U L 6 6 PAGE -- ...-- -- r U n G . DOCUMENT NUMBER, OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD 6 5 ICD9766-003 I - - 501-66-0045 501-66-0327 R 2 R 3 - SEE-DWG PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 02-10-66 LO-FA PHY I C D S - I C PNEU CONSOLE RKS 1-2-3+4 ICD-CCBD 5 0 1 - 6 5 - 6 1 09-1 5 - 6 5 LO-FA PHY I C D PNEU CONSOLES 596.7 ICD-CCBD 5 0 1- 6 5 - 3 4 08-09-65 LO-FA PHY I C D S - I C PNEU CHECKOUT RKS 1-2-3+4 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA PIPING CRITERIA S-IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 12-09-65 LO-FA 210-390 P I P C R I T S - I C F L U S H + PURGE U N I T SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 7 . 02-07-66 LO-FA 010-390 - PHY I C D + P I P E C R I T S I I L E A K DETECT SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 4 , I RN-CCBD 5 0 1 - 6 6 - 0 2 7 4 0 2 - 1 0-65 LO-FA 020-220 MSFC-ED' 4 8 S-IC PNEU CONSOLE SET A S - I 1 STAGE GSE PLACEMENT ON MBL LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 - PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T -------- -------- ------ -------------- ------ SEE B A S I C NUMBER FOR R E V I S I O N p T I T L E o E T C . - J 65ICD9775 SCHED ACTUAL R E L DATE R E L DATE P A N E L MO DA YR MO DA YR CODE 220-390 KSC-K-0 220-390 MSFC-ED . KSC-EDV MSFC-ED �APOLLO INTERFACE CONTROL DOCUMENT COG IAOL PAGE 17, DATE 2 9 J U L 6 6 -- --- -- D S -- DOCUMENT NUMBER, OR R E V I S I O N NOTICE -- DOC REV ACTUAL SCHED REL DATE REL DATE PANEL MO D A YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... --------------I---- I? I IRN-CCBD - - - J 65ICD9766 . - -------- s --09-- PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T Y - --------------- --- ---- 501-66-0292 06-21-65 LO-FA 220-390 KSC-P+VE P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 02-1 0-66 LOFA 220-390 MSFC-EDV PHY I C D S - I C I N E R T P R E F I L L + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 7 09-1 5-65 LO-FA 220-390 MS FC-EDV PHY I C D S - I 1 PNEU CONSOLES S7-41B/SAT ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA PHY I C D APS PNEU CONS DSV-4B-436/SAT ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 PHY I C D S I I PNEU CONSOLE S7-41C/SAT ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 . IRN-CCBD 5 0 1 - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 l D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBO 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A7-71/SAT ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S - I 1 V V V . 220-390 , V V PNEU SYS/SATURN V 06-25-65 LO-FA 220-390 02-11-66 LO-FA 220-390 i �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 6 6 .. . -- --- 1 ; t c S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E R R 2 3 J 65ICD9751 c AS -- R DOC REV - 1 - J 65ICD9758 - CONTO PAGE SCHED ACTUAL R E L D A T E R E L DATE P A N E L no D A YR MO D A YR CODE -------- DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD IRN-CCBD 1 505 ----- IAOl bb-Q--- ---- u- PREPARIi I N T E R F A C E AREAS CENTER OR CEI NUMBERS ACTIVIT' -------. ----------we-- 501-66-0178 501-66-0281 501-66-0288 UMB + S E R V I C E CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 3 FORWARD U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 4 06-1 8-65 LO-FA 040-390 06-18-65 LO-FA 090-390 KSC-P+VE * KSC-P+VE PHY I C D S - I V B PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 V 06-21-6s LO-FA 220-390 KSC-K-01 PHY I C D S - I V B PNEU CONS D S V - 4 B - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V 06-2 1-65 LO-FA 220-390 KSC-P+VI 01-28-66 LO-FA 020-390 KSC-P+Vl 06-21-65 LO-FA 220-390 KSC-P+VI 0Q-15-65 LO-FA 220-390 HSFC-EDk 09-1 5-65 LO-FA 220-390 HSFC-EDV P I P I N G CRITERIA S-IVB ICD-CCBD 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1-66-0374 PNEU CONS SET L C 3 9 PHY I C D . S - I V B H T EXCH D S V - 4 B - 4 3 8 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 6 V PHY I C D I U C O O L I N G U N I T + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 PHY I C D I U PNEU CONS,+ ICD-CCBD 5 0 1 - 6 5 - 4 8 P I P I N G CRITERIA �APOLLO I N T E R F A C E CONTROL DOCUMENT AS DATE 2 9 J U L 66 -- --- -- DOCUMENT NUMBER, OR R E V I S I O N NOTXCE .................... DOC REV --- ........................................ IRN-CCBD 65 ICD9745 I? R R - 1 2 3 - - 65ICD9749 R R R - 2 3 5 6 5 1CD9750 5 0 5 CONT. ----- DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD LOG PAGE 1 7 -- SCHEO ACTUAL R E L D A T E R E 4 DATE P A N E L MO DA YR NO D A YR CODE -------- -------- -o---- PREPARINC I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T " v 1 T Y -------------- --. ---- 501-66-0290 501-66-0296 501-66-0378 PHY I C D L A U VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 7 IRN-CCBD 5 0 1-66-0190 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO IRN-CCSD ENTERED FWD U M B / L C 3 9 G S E 08-09-65 LO-FA 010-390 KSC-P+VE 06-28-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S I I LOX DISCONNECT ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-21-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 6 06-2 1-65 LO-FA 020-390 KSC-P+VE 06-28-65 LO-FA 020-390 KSC-P+VE 06-2 1 - 6 5 LO-FA 040-390 KSC-P+VE UMR + SERV CONNECTIONS S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRiJ-CCBD 501-66-0111 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 3 INTERM LH2 DISC U M B I L I C A L + S E R V I C E CONN S - X I ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED FORWARD , , - UMB + SERV CONNECTIONS S - I V B AFT �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE D A T E 2 9 JUL 6 6 -- --- -- S DOCUMENTNUMBER9 OR R E V I S I O N N O T I C E DOC REV -- - ------------------- --R 1 A 651CD9407 R DOCUMENT T I T L E OR CCBD NUMBER ...................................... IRN-CCBD - 1 - - - ----I--- PREPARII INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T ' - ------.---------------- ----I 501-66-0041 FUNCT I N T F F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED 05-19-65 LOPG 000-260 KSC-K-Dl P I P C R I T APS PROP S E R V I C I N G SAT V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-EDV U M B AND SERV CONN P L A T E 3-4 S I C AFT 08-10-65 LO-FA 010-210 KSC-P+VE 010-210 KSC-P+VE ICD-CCBD IRN-CCBD IRN-GCBD IRN-CCBD - SCHED ACTUAL REL D A T E REL D A T E PANEL MO DA YR MO D A YR CODE 501-65-40 501-66-0299 501-66-0289 501-66-0378 UMB + SERV CONNS P L A T E NO 1-2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT 08-1 8-65 LO-FA UMB + SERV CONNS P L A T E NO 3-2 ICD-CCBD 5 0 1-65-39 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT 08-10-65 LO-FA M O T I O N ENV AFT UMB P L A T E S l r 2 9 + 3 S - I C ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-10-65 LO-FA PHY I C D L A U VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 6 08-09-65 LO-F A JNTK U M B / L C 3 9 GSE I . �APOLLO INTERFACE CONTROL DOCUMENT LOG IAOl PAGE 1 - DATE 2 9 J U L 66 -- --- -- D .- S - DOCQJMENTNUMBERo OR R E V I S I O N N O T I C E .................... -. DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - - PREPARIM( INTERFACE AREAS CENTER OR C E I NUMBERS AC" ITY - ---9--.-- -ID---- S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSFC-KSC FUNCT I N T F F L U I D REQMTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS L H 2 SYS SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS LOX S Y S SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 06-03-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 06-15-65 LOPG 010-250 KSC-P+VE ICD-CCBD - SCHED ACTUAL R E L DATE REL DATE PANEL MO D A Y R MO DA YR CODE ----C)--- ---P--O-_D-P-PU ---YO--. 501-66-0082 SYS SAT V �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl D A T E 2 9 JUL 6 6 PAGE -- --- -- C i~ G DOCUMENT NUMBERp OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD I - - - PREPAR! I N T E R F A C E .AREAS CENTER ACTXVIl OR C E I NUMBERS --------------- ------- 501-66-0136 WIND LOAD A L L E V I A T I O N S Y S F A C I L TO L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E ESE ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - SCHED ACTUAL R E L DATE R E L DATE P A N E L MO DA YR MO DA YR CODE 09-0 1-66 03-09-66 LOFC 000-040 MSFC LO-EL 2 2 0-3 9 0 MSFC-AS 220-390 HSFC-AS L V E S E TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 L V E S E / 6 0 A C POWER REQUIREMENTS ICD-CCBD 5 0 1-66-0174 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 0 2 - 1 1-66 LO-EL 220-370 HSFC-AS L V ESE T O I N S T R SYSTEM ICD-CCBD 501-66-0084 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 0 2 - 1 1-66 LO-EL 220-290 MSFC-AS MSFC COUNT CLOCK TO KSC T I M I N G L C - 3 9 ICD-CC8D 5 0 1-65-84 NO IRN-CCBD ENTERED 08-14-65 LOEL 200-390 HSFC-AS L V ESE TO K S C DATA ME.ASUREMENTS 0 2 - 1 1-66 LOEL 220-290 HSFC-AS LOW BAY ESE TO I N S T R U S Y S + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 G2-11-66 LO-EL 220-290 HSFC 02-11-66 LO-EL 220-290 MSFC-AS �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG XA01 P A G E 17 DATE 2 9 J U L 66 -- -- --- - D S DOCUMENT NUMBERo OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER - - ------------------- --- ---------------------------------------NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD J 65ICDG302 - LC34/37/39 A MOCK-UP J 651CD8311 - - _------ -------- ----- PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT iTY - ----u-------c--------- ENTERED ENTERED ENTERED CMD MOD ACCESS ARM C A B L I N G VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED J 65ICD8304 SCHED ACTUAL R E L D A T E R E L DATE PANEL MO D A Y R MO DA YR CODE 2 3 AFRM 9 T O ACCESS ARM HHT RM 11-17 - 6 4 LOFA 230-340 KSC-D 11-18-64 LOFA 230-300 MSC-FO 03-1 7 - 6 5 LOFA 230-300 KSC-DE C / M ACCESS ARM ADPT HOOD TO S / C I N T F RE8 11-04-65 LOFA 'LOO-300 MSC-EDV PHY I N T F R E T R A C T I O N NECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER 12-10-65 LO-FA 110-300 KSC-ECV SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC L C 3 9 VAB H I G H BAYS T O L / V ESE/GSE 11-19-65 LOFC 220-390 KSC-F LC 3 9 VAB LOW BAY AREA T O L/V-ESE/GSE TCD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-EDV-2 L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-EDV-2 L C - 3 9 PAD AREA L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EDV-2 04-05-66 LO-FC 220-390 MS FC -- S - I C / M L HOLD DOWN ARMS P H Y S I C A L REQMTS ' 220-390 ' MSFC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOP DATE 2 9 JUL 66 -- ------ PAGE SCHED ACTUAL REL DATE R E L DATE PANEL MO DA Y R #O DA YR CODE C H DOCUMENT NUMBER9 DR R E V I S I O N N O T I C E --_ _ .................... r DOC REV -a- DOCUMENT T I T L E OR CCBD NUMBER ENTERED L C 3 9 A M L P I P C R I T 4 I N T F LOC S / C NO IRN-CCBD ENTERED NO 1RN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED F L SYS - LC39-LUT - L C 3 9 PHY I N T F C GOX COND PNL L E A K TS U N I T GSE CABLES-GAS NO IRN-CCBD - - ACCESS ARM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD KSC-EDV N I T SYS KSC-DE KSC-EDV ENTERED + SERV MODULE CABLE REQMTS ENTERED ENTERED ENTERED ENTERED LEM U M B I L I C A L AND T E S T CABLES FOR L C 3 9 NO IRN-CCBD ENTERED LC/34/37/39 T I M I N G + COUNTDOWN D I S T KSC-EDV 09-22-64 LO-FC 230-340 POWER RECo + CONN 11-29-65 LOFC 230-347 KSC-EDV FUNCT I N T F REQNTS E C S MC L E H S / C GSE 05-03-65 LOPG 230-300 KSC-K-O LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 10-01-64 LOFA 230-340 MSC-FO- A S/C - --------------- ------ - _ - - - - - - - - - - - - - - - - - - - - - - - - - I--0 . ----I ------- NO IRN-CCBD - -------- PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT A-C- S M SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED , 8 l C 3 7 / 3 9 L E H SWG ARM UMB DISC A14-172 KSC-EDV �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 17: DATE 2 9 J U L 66 -- --- -- D S DOCUYENT NUMBER, OR R E V I S I O N N O T I C E --. DOC REV - DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L D A T E R E L . D A T E PANEL MO DA YR MU DA YR CODE PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T " ' T Y -------- -------- ------ --------------- ---P ----- L C 3 9 / M S S P I P C R I T + I N T F LOC LEM F L D SYS 12-02-65 LOPG 140-390 KSC-EDV L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD 01-12-65 LOFC 230-390 KSC-F FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO IRN-CCBD ENTERED 03-19-65 LOPG 100-390 KS C-K-CT - FUNCT I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-EDV - FUNCT I N T F REQMTS GN2 L C 3 9 A S I C GSE 05-02-66 LOPG 100-390 KSC-K-DT L C 3 9 A S / C GSE FUNC !NTF (22-09-66 LOPG 230-390 KSC-EDV 02-10-66 L/-FC 230-300 KSC 03-19-65 LOPG ' 100-390 KSC-K-DT 11-05-64 LO-FC 230-390 MSC-NAA - - LC-39 ENTERED ENTERED REQVGOX PAD 8 S / C FUNCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE B L C 3 9 L U T GSE SYSTEMS AFRM C O N F I G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NU IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED . �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl DATE 2 9 J U L 66 PAGE I -- --- -- D S DOCUMENTNUMBERo 3 R R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD A 65ICD7166 A 65ICD7167 - PREPAR I F I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT) ------we -----d--------- -------- ------ - ------- ENTERED ENTERED ENTERED FUNCT I N T F REQS ECS L C 3 9 V A B S/C-GSE 03-19-65 LOPG 100-390 KSC-K-DT FUNCT I N T F RQMTS ECS L C 3 9 / V A S L E N SC GSE 05-03-65 LOPG 230-390 XSC-K-DT L C 3 9 LCC F A C I L I T Y S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 03-05-65 230-390 KSC-F ESE/GSE A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - SCHED ACTUAL R E L D A T E R E L D A T E PANEL HO DA YR MO D A YR CODE LC39 PIPING NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD G R I T + I N T F LOC S / C ENTERED ENTERED ENTERED ENTERED F L D SYS 01-25-65 LOFC 230-390 KSC-F 03-03-65 LOPG 100-200 KSC �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE If DATE 2 9 J U L 66 -- --- -- D 5 DOCUMENT NUMBERp OR R E V I S I O N N O T I C E -- DOC REV - DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L D A T E REC DATE PANEL M O D A YR MO D A YR CODE PREPAR I N ( I N T E R F A C E AREAS CENTER OR C E I N U M B E R S AC ITY - 03-23-65 LOFC 230-390 KSC-F A L C 3 9 SAT V TRANSP ROUTES -S/C 03-1 5-65 LOFC 230-390 KSC-ECV-; A L C 3 9 SAT V VEH STAGE + S / C M I S A L I G N M E N T 08-13-65 LOFC 100-390 KSC-ECV-; 02-08-66 LOEL 04-28-65 LOFC L C 3 9 OPNL T V SYS-FAC-S/C A ~ NO NO NO NO NO NO NO NO NO NO NO NO NO - S/C ~ csn 3 9 9 LEM TO FACILITY IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED IRN-CCBD ENTERED ESE/GSE CABLES GSE TO HAZARD PROOF MON S Y S T 9 L C - 3 9 A L C 3 9 VAB H I G H BAY AREA T O S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl DATE 2 9 J U L 66 PAGE -- --- -SCHED ACTUAL R E L D A T E R E L DATE PANEL MD DA YR HO DA YR CODE C I DOCUMENT NUMBER9 OR R E V I S I O N NOTICE I DOC REV G DOCUMENT T I T L E OR CCBD NUMBER --- ------------------- --- ..................................... A 16331-63~107350 A 16331-63A107393 ' - * +++ A 403437545 50M36801 -0--- 03-18-65 EI 300-230 MSG 08-12-65 €1 300-100 HSC L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 12-15-65 €I 220-210 MSFC-AS L V E S E TO LAUNCH EQUIPMENT ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 12-09-65 €1 220-210 HSFC-AS 03-11-66 €-I 000-100 MS FC-A! 11-30-67 EI 000-220 MSFC 0 3 - 1 5-66 M-NF 040-090 MSFC-M- 01-28-65 LOFC 230-390 KSC-F 02-02-65 LOFC 230-390 KSC-F 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 ELEC ICD ICD-CCBD COMP INTF A C E SIC-L/V 501-66-0085 - SC E S E TO L V E S E - DEF SATURN S A - 5 0 5 - ------------- ----.=.--- A SOFTMARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - -------- PREPAR: I N T E R F A C E AREAS CENTER AGTIVIl OR C E I NUMBERS COMP I N T E R F A C E APOLLO S C - 1 0 5 ELEC INT EDS CHECKOUT SCHEMATICS + APOLLO S C - 1 0 5 DES O f SATURN S A - 5 0 5 ICD-CCBD 501-66-0277 I C D SATURN I B / V CONTROL RATE GYRO PKG L C 3 9 S I T E P L A N + GENL ARRANGE-S/C NO IRN-CCSD ENTERED GSE L C 3 9 DATA TRANS S Y S ( Q 1 D E BAND) NO IRN-CCBD ENTERED . A 65 ICD7002 - L C 3 9 OPNL INTERCOM S Y S - S I C 65IC07003 - L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G ESE/GSE S/C --0--0- EDS . KSC �A P O L L 0 I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 DATE 29 J U L 66 -- --- -- D S DOCUMENT NUMBER9 OR R f V I S I O N NOT I C E - DOC REV -- - -------------------- --- - DOCUMENT T I T L E OR CCBD NUMBER -_-_---------PP------------------------ - PREPARIN I N T E R F A C E A R E A S CENTER OR C E I NUMBERS ACT'VITY - -------- -------- ----- -------------- -- L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 8 L A U VEH/SPACECRAFT F U N C T I O N A L REP ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 B ENVELOPE L E M / S - I V B / I U ICD-CCBD 5 0 1 - 6 6 - 0 0 9 9 - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA Y R MO D A Y R CODE CLEARANCE P H Y S I C A L INSTRUMENT U N I T 10 SPACECRAFT PHYS REQ NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 8 0 IRM-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT T O Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 T RN-C CBD 50 1 - 6 6 - 0 2 4 2 PHYS REQ 8 SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 LV TO S C ( C S M - 1 0 4 e L E M S ) I N S T R ICD-CCSD 5 0 1 - 6 6 - 0 0 7 0 IRN-CCBD 5 0 l - 6 6 - 0 3 9 5 + COMM I N T F 01-28-66 IC 000-100 KSFC-AST .. , 0 D E S I G N C R I T E R I A FOR SATURN V ONBOARD EDS ICD-CCBD 5 0 1 - 6 6 - 0 0 7 8 08-06-65 C-S 000-LO0 MSFC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 JUL 6 6 PAGE -- --- -- DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DOC REV 1 ' ; _ -------------------- --- ,__ S I 65ICD9776-001 DOCUMENT T I T L E OR CCBD NUMBER -------------Q-------O-----O----ba----- - PHY I C D P I P E C R I T S I C FMD UMB SERV UN SV ICD-CCBD 5 0 1 - 6 6 - 0 1 8 0 * SEE B A S I C NUMSER FOR R E V I S I O N o T I T L E p E T C . - PHY I C D ICD-CCBD IRN-CCBD IRN-CCBD + SCHED ACTUAL R E L DATE R E L D A T E P A N E L HO DA YR MO D A YR CODE PREPARI! I N T E R F A C E AREAS CENTER OR CEI NUMBERS A C Y l V I T l ------I- -----a------*-- .++ .++ 66ICD7009 A $OM90504 - LC-39 L C 3 9 S/C Doc. POWER S U P P L I E S F L I G H T MECHANICS P A N E L ------ - LO-FA 010-220 -------MSFC-ED) SEE-DWG P I P C R I T HAZ GAS ANALYZER S A T V . 501-66-0100 5 0 1-66-0377 501-66-0315 HAZARD PROOF ING-S/C ---me--- 0 2 - 1 0-66 A L C 3 9 M L PHY LOC PORT I U WATER ACCUM CART ICD-CCBD 5 0 1 - 6 6 - 0 2 0 7 66ICD7007 I 01-20-66 02-04-66 LO-FA 220-000 MSFC-ED\ 03-02-66 LO-FA 220-390 KSC-EDV 02-08-66 LOFC 230-390 KSC 230-390 KSC-EDV- LOFC , �APOLLO INTERFACE CONTROL DOCUMENT LOG P A G E 1C DATE 2 9 J U L 66 -- -- --- -- CI .- DOCLIMENTNUMBER, OR R E V I S I O N N O T I C E DOC REV -S -------------------- --- DOCUMENT T I T L E OR C C B D NUMBER -------------PP----__OO--CIP-OP-P--P----- ICD-CCBD IRN-CCBD 65 I C D 9 7 6 6 - 0 0 3 + - SCHED ACTUAL R E L DATE REC DATE P A N E L MO DA YR MO D A Y R CODE ---PO--- -PO----- PREPARIN( I N T E R F A C E A R E A S CEWTER fTY OR C E % N U M B E R S A C ' ------ --------------- e>-------- 50 1-66-0045 501-66-0327 SEE-DWG S E E B A S I C NUMBER F O R R E V I S I O N 9 T I T L E p E T C o PHYS I C D S - I C HYDRAULIC U N I T L C 3 9 ICD-CCBD 501-66-0183 02-10-66 LO-FA 220-390 KSC-K-DT - PHY I C D S - I C PNEU C O N S O L E RKS 1 - 2 - 3 + 4 ICD-CCBD 501-65-61 09-1 5-65 LO-FA 220-390 KSC-K-Df - PHY I C D P N E U C O N S O L E S 5 * 6 9 7 + 8 S - I C ICD-CCBD 501-65-34 08-09-65 LC-FA 220-390 KSC-P+VE - PHY I C D S-ZC PNEU CHECKOUT RKS 1-2-394 ICD-CCBD 501-65-46 09-24-65 LO-FA 220-390 NSFC-EDV P I P I N G CRITERIA S-IC ICO-CCBD 501-66-0046 IRN-CCBD 501-66-0306 02-07-66 LO-FA 220-280 MSFC-P+VE A S-I1 STAGE G S E PLACEMENT ON MBL LAUNCHER ICD-CCBD 501-66-0129 IRN-CCBD 501-66-0129 12-09-45 LO-FA 210-390 KSC-EDV - P I P C R I T S - I C F L U S H + PURGE U N I T S A T V ICD-CCBO 501-66-0047 02-07-66 LO-FA 010-390 MSFC-EDV PHY I C D ICD-CCBD I RN-CCBD IRN-CCBD 02-10-65 LO-FA 020-220 HSFC-EDV - - 4 PNEU CONSOLE S E T P I P E C R I T S I I ' L E A K DETECT S Y S 501-66-0155 501-66-0264 501-66-0274 ' - �APOLLO . I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 PAGE 1 -- --- -- f S DOCUMENTNUMBER, dK R E V I S I O N N O T I C E R DOC REV 1 DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD J 651CD9759 I - - - SCHED ACTUAL R E L D A T E REL DATE PANEL HO DA YR MO D A YR CODE PREPARIN I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y - 501-66-0292 06-21-65 LO-FA 220-390 KSC-P+VE P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 02-10-66 LOFA 220-390 HSFC-EDV PHY I C D S - I C I N E R T P R E F I L L + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 7 09-1 5-65 LO-FA 220-390 MSFC-EDV PHY I C D S - I 1 PNEU CONSOLES S 7 - 4 1 B / S A T ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 06-2 5-65 LO-FA 220-390 KSC-P+VE 02-1 1-66 LO-FA 220-390 HSFC-EOV PHY I C D APS PNEU CONS D S V - 4 B - 4 3 6 / S A T ICD-CCBD 5 0 1- 6 6 - 0 1 0 4 PHY I C O S I I PNEU CONSOLE S 7 - 4 1 C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 501-66-0128 IRN-CCBD 501-66-0294 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 l D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T TCD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CC8D 5 0 1 - 6 6 - 0 1 3 1 V V V V V P I P I N G C R I T E R I A S - I 1 'PNEU S Y S I S A T U R N V ' . KSC-P+VE �APOLLO INTERFACE C O N T R O L DOCUMENT LOG IAOl PAGE 1 DATE 2 9 JUL 66 -- --- -- I 0 ; S DOCUMENT NUMBER9 OR REVISION NOTICE - DOC REV SCHED ACTUAL REt DATE REL DATE PANEL M O DA Y R M O D A Y R CODE DOCUMENT TITLE OR CCBD NUMBER -------- ---POP-- PIP--- PREPARIY INTERFACE A R E A S C E N T E R OR CEI N U M B E R S Ar V I T Y -P---C----OO--P- --.s----- ICD-CCBD 50 1-66-0178 IRN-CCBD 501-66-0281 IRN-CCBD 501-66-0288 J 65ICL39751 R - 1 J 651~09753 - - - UMB + SERVICE CONNECTIONS S-IV8 FORWARD ICD-CCBD 50 1-66-0177 IRN-CCBD 501-66-0283 06-1 8-65 LO-FA 040-390 KSC-P*Vf UMBILICAL + SERVICE CONNECTIONS IU ICD-CCBD 501-65-35 IRN-CCBD 501-66-0285 I RN-CCBD 50 1-66-0286 06-18-65 LO-FA 090-390 USC-P+V1 220-390 KSC-K-DI 220-390 KSC-P+YI PHY ICD S-IVB PNEU CONS DSV-48-4321SAT ICD-CCBD 501-66-0107 V 06-21-65 LO-FA PHY ICD S-IVB PNEU CONS DSV-48-433/SAT ICD-CCBD 501-66-0105 V 06-21-65 LO-FA PIPING CRITERIA S-IVB PNEU CONS SET LC39 ICD-CCBD 50 1-66-0043 IRN-CCBD 501-66-0374 01-28-66 LO-FA 020-390 KSC-P+V1 PHY ICD S-IVB HT EXCH DSV-48-438/SAT ICD-CCBD 501-66-0106 06-21-65 LO-FA 220-390 K 09-15-65 LO-FA 220-390 MSFC-ED' V PHY ICD IU COOLING UNIT + PIPING CRlT ICD-CCBD 50 1-65-49 IRN-CCBD 501-66-0376 . , -. , - PHY ICD I U PNEU CONS ICD-CCBD 501-65-48 PIPING CRITERIA \P+V 09-15-65 LO-FA 220-390 MSFC-ED' �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 2 9 JUL 66 PAGE 1 -- --- -- f DOCUMENT NUMBERp DR R E V I S I O N N O T I C E - DOC REV SCHED ACTUAL R E L DATE R E L DATE P A N E L MO DA Y R MO D A YR CODE __ _ __--------------------- ........................................ S DOCUMENT T I ' T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD IRN-CCBD IRN-CCBD - -------- ------- ------ PREPARIh I N T E R F A C E AREAS CEMTER OR C E I NUMBERS ACTIVITY - ----el -Q------------ 501-65-36 501-66-0290 5 0 1-66-0296 5 0 1-66-0378 PHY I C D L A U VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO IRN-CCBD ENTERED FWD U M 8 / L C 3 9 GSE 08-09-65 LO-FA 010-390 KSC-P+VE 06-28-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S I I L O X DISCONNECT 1CD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 501-66-0127 06-21-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 6 LH2 DISC 06-21-65 LO-FA 020-390 S-I1 FORWARD 06-2 8-65 LO-F A 020-390 KX-P+VE 06-21-65 LO-FA 040-390 KSC-P+VE - . U M B + SERV CONNECTIONS 5-11 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 3 INTERH ' - - U M B I L I C A L + S E R V I C E CONN ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED UMB + SERV CONNECT1 ONS S - I V B AFT , KSC-P+VE �9 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 6 DATE 2 9 J U L 66 -- -- --- -- DOCUMENT NUMBER, OR R E V I S I O N N O T I C E .................... DOC REV SCHED ACTUAL R E L D A T E R E L . D A T E PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER -------- --- ....................................... - - --em---- PREPARING I N T E R F A C E AREAS CENTER OR CEI NUMBERS ACT TTY - ------ --------------- 06-15-65 LOPG 010-250 K!jc-P+VF FUNCT I N T F F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED 05-19-65 LOPG 000-260 KSC-K-DT P I P C R I T APS PROP S E R V I C I N G SAT V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-EDV UHB AND SERV CONN P L A T E 3 - 4 ICD-CCBD 5 0 1 - 6 5 - 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 08-10-65 LO-FA 010-210 KSC-P+VE 08-1 8-65 LO-FA 010-210 KSC-P+VE SYS SAT V FUNCT I N T F F L U I D REQMTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 1 S I C AFT uMB + SERV CONNS P L A T E NO 1 - 2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC UMB + SERV COMNS P L A T E NO 3 - 2 ICD-CCBD 5 0 1 - 6 5 - 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT . AFT M O T I O N E N V A F T UMB P L A T E S 1 1 2 9 + 3 S - I C ICD-CCBD 5 0 1-66-0042 .IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 PHY IC!: 'LAU VEH S - I C ' XNTK U M B / L C 3 9 GSE 08-10-65 LO-FA 08-10-65 LO-FA 08-09-65 LO-FA 010-210 MSF . '+VE �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 66 AS -- --- -- 504 9. r '. DOCUMENT NUMBER, OR R E V I S I O N N O T I C E PAGE CONTO -I--- D IAOl DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD - - - SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO DA YR CODE PREPARI INTERFACE AREAS CENTER OR C E I NUMBERS A C T I Y I T -------- ------- ------ ------------- ------- 501-66-0171 LOU BAY^ ESE TO I N S T R SYS AND REC ICD-CCBD 5 0 1 - 6 6 - 0 0 8 2 02-1 1-66 LO-EL 220-290 MS FC-AS' S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSFC-KSI FUNCT I N T F F L U I D REQMTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG Of0-250 KSC-P+Vi F U N C T I N T F F L U I D REQMTS GN2 SYS SAT V 06-28-65 LOPG 010-250 KSC-P+Y 06-28-65 LOPG 010-250 KSC-P+V FUNCT I N T F F L U I D REQMTS L H 2 SYS SAT V NO IRN-CC8D ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG 010-250 KSC-P+VI FUNCT l N T F F L U I D REQHTS LOX SYS S A T V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 . 06-03-65 LOPG 010-250 KSC-P+VI NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD ENTERED ENTERED ENTERED FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED ' �APOLLO INTERFACE' CONTROL DOCUMENT LOG AS DATE 2 9 J U L 66 -- D S -a- -- DOCUFrENT NUMBER, OR R E V I S I O N N O T I C E 65 ICD9100 DOC REV - 65ICD9142 - DOCUMENT T I T L E OR CCBD NUMBER - A 65ICD9205 A 65ICD9240 - --- SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE PREPARING I N T E R F A C E AREAS C E N T E R OR C E I NUMBERS ACTk' f Y - L C - 3 9 PAD AREA L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EPV-2 S - I C / M L HOLD DOWN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC 220-390 MSFC LOFC 000-040 MS FC 03-09-66 LO-EL 220-390 MSFC-ASTR L V ESE TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 08-14-65 LOEL 220-390 MS FC-ASTW L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 02-1 1-66 LO-EL ' 220-370 PlS FC-ASTR L V E S E T O I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-1 1-66 LO-EL 220-290 MSFC-ASTR MSFC COUNT CLOCK T O KSC T I M I N G LC-39 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED 08-14-65 LOEL 200-390 MS FC-ASTR L V ESE TO K S C DATA MEASUREMENTS 02-11-66 LOEL 220-290 HSFC-ASTR LOW BAY ESE T O I N S T R U S Y S + REC 02-1 1-66 LO-EL 220-290 MSFC WIND LOAD A L L E V I A T I O N SYS F A C I L TO L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E ESE ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - PAGE 1 5 9 5 0 4 CON?, ----- 09-01-66 �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS - 5 0 4 D A T E 2.9 J U L 60 ----- -- --- -- G ___ _ DOCUMENTNUMBER, OR R E V I S l O N NOTICE DOC REV __---------------- --- - DOCUMENT T I T L E OR CCBD NUMBER --------------------------------.-.-------LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD B L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD J 651CD8302 - J 65ICD8304 J 65ICD8311 LC34/37/39 - - - -------- -------a- PREPAR 1 I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIl ------ -------------- ------- 10-01-64 LOFA 230-340 NSC-FO- SWG A R M UMB D I S C A l 4 - 1 7 2 ENTERED ENTERED ENTERED 03-07-66 LOFA 230-340 KSC-EDV CMD MOD ACCESS ARM C A B L I N G 11-17-64 LOFA 230-340 KSC-D 11-18-64 LOFA 230-300 HSC-FO 03-17-65 LOFA 230-300 KSC-DE 23 AFRM 9 T O ACCESS ARM WHT RM C / M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 MSC-€0'1 PHY I N T F R E T R A C T I O N MECH 8-BALL COVER 12-10-65 LO-FA 110-300 KSC-ED\ SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC 220-390 MS FC L C 3 9 VAB H I G H BAYS TO L / V ESE/GSE 1 -1 9 - 6 5 LOFC 220-390 RSC-F LC 3 9 V A 8 LOW B A Y AREA TO L/V-ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-EDV 02-14-66 LO-FC 220-390 KSC-EDV ICD-CCBD - SCHED ACTUAL REL DATE R E L DATE P A N E L MO DA YR MO DA YR CODE S M SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED VERT STOP FOR L E S ACCESS ARM NO 1RN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP PAGE CONY, C D S IAOl 5 0 1-66-0164 4 - L C 3 9 HSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 �v APOLLO I N T E R F A C E CONTROL DOCUMENT LOG P A G E 1: DATE 29 J U L 66 -- --- -- D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E -. DOC REV SCHED ACTUAL R E L D A T E RE& DATE PANEL MO DA YR MO DA YR CODE NO NO NO NO NO NO 8 9 10 11 14 16 - - IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ----.----. ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED L C 3 9 A ML P I P C R l T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED LC39-LUT - -------- -------- ------ -------------- DOCUMENT T I T L E OR CCBD NUMBER -- - -------------------- --- ........................................ R R R R R R PREPARINl I N T E R F A C E AREAS CENTER OR C E I NUMBERS At' 'ITY GSE CABLES-GAS F t SYS N I T SYS L C 3 9 PHY I N T F C GOX COND, PNL L E A K TS U N I T NO IRN-CCBD ENTERED 11-1 7 - 6 4 LOFA 07-22-65 LOFA . 230-390 KSC-EDV 230-390 KSC-DE 230-390 KSC-EDV I - - - ACCESS ARM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD 09-22-65 LOFA 230-390 KSC-EDV 08-20-65 LOFA 230-390 KSC-EDV T I M I N G + COUNTDOWN D I S T 09-22-64 LO-FC 230-340 + CONN 11-29-65 LOFC 230-347 KSC-EDV- 05-03-65 LOPG 230-300 KSC-K-DT ENTERED ENTERED ENTERED ENTERED LEM U M B I L I C A L AND T E S T CABLES FOR LC 39 NO IRN-CCBO ENTERED LC/34/37/39 A S/C - + SERV MODULE CABLE REQMTS A-Ce POWER REC- FUNCT I N T F REQMTS ECS MC LEM S / C GSE - �& P O L L O 1 N T E W F ACE C O N T R O L D O C U H E N T LOG PAGE 1 5 5 --- SCHED ACTUAL REL DATE REL DATE PANEL H O D A Y f i MO D A YR CODE ----...--- - bSliD7t6m7 FuNGT I N T F R Q H T S ECS L C 3 9 / V A 8 L E H SC G S E L C 3 9 LCC F A C I L I T Y S I C ESE/GSE NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D ..- ?iC. r . 7 r , r 100-390 KSC-K-DT 05-03-65 LOPG 230-390 KSC-u-DT 230-390 KSC-F 230-390 KSC-F 01-25-65 LOFC < ENTERED FLD SYS I LOPG e LC39 PIPING C R I T + I N T F LOC S / C CTIV! -------------- A---------- 03-19-65 IZ%i-C,S?l; E ? i f E ? E j NO I R N - C C f i D - - OR C E I NUMBERS --I--- 03-05-65 A L C 3 9 MAT-ESE/GSE NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C S D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D YCI T9N-CcS3 E h f T E P E D ,." -; ' 4.- * *I, . * - * * < <., < PREPARING I N T E R F A C E AREAS CENTER 09-03-65 LOPG �v A POLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 151 DATE 2 9 J U L 66 -- --- -- D S DOCUMENTNUMBERp OR R E V I S I O N N O T I C E -- DOC REV DOCUMENT T I T L E OR CCBD NUMBER - - -------------------- --- ....................................... NO NO NO NO NO NO NO - IRN-CCBD IRN-CCBD TRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD I N T F RQMTS ECS L C 3 9 / V A B LEM SC GSE -------- ------ -------------- ---- ,----. L C 3 9 P I P I N G C R I T + I N T F LOC S / C 03-19-65 LOPG 100-390 KSC-K-DT 05-03-65 LOPG 230-390 KSC-K-DT 230-390 KSC-F 230-390 KSC-f 03-05-65 L C 3 9 LCC F A C I L I T Y S I C ESE/GSE NO .I RN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED -- a PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT'. ' T Y ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED FUNCT I N T F REQS ECS L C 3 9 V A B S/C-GSE FuNCT SCHED ACTUAL R E L DATE R E L . D A T E P A N E L MO DA YR MO D A YR CODE F L D SYS 01-25-65 LOFC 09-03-65 LOPG ' �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 AS 504 - CONTo . v O DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC RE V --- DOCUMENT T I T L E OR CCBD NUMBER --_-O--O---a-----O-O--_--OI--CI---.O-.P--- NO NO NO NO f 65ICD7468 - * 65 I C D 7 6 0 0 - A 651CD7666 - C 65ICD7567 C 651CD7568 C 651CD7569 IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ..,. ,----- c - IAOl SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE -------- ------- 0-0--0 PAG! PREPAl I N T E R F A C E AREAS CENTEI OR C E I NUMBERS ACTIV -----O--------- ----. ENTERED ENTERED ENTERED ENTERED P I P C R I T + I N T F LOC LEM F L D SYS 12-02-65 LOPG 140-390 KSC-ED 01-12-65 LOFC 230-390 KSC-F FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO IRN-CCBD ENTERED 03-19-65 LOPG 100-390 FUNCT I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-ED\ FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPC 100-390 KSC-K-I L C 3 9 A S / C G S E FUNC I N T F REQVGOX 02-09-66 LOPC 230-390 KSC-ED' 02-10-66 L/-FC 230-300 KSC 03-19-65 LOPG 100-390 KSC-K- 11-0 5-64 LO-F C 230-390 HSC-NA LC39/MSS L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD LC-39 ENTERED ENTERED PAD B S / C FUNCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE B L C 3 9 .LUT GSE SYSTEMS AFRM C O N F I G NO IRN-CCSD ENTERED NO I R N - C C B D ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS D A T E 2 9 J U L 66 -- --- -- ! D 7 . ._- - DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV ---------------__--- A 65ICD7002 . 504 ----- CON?', DOCUMENT T I T L E OR CCBD NUMBER -------------------__Y_---------------- - L C 3 9 OPNL INTERCOM SYS-S/C IAOl ESE/GSE PAGE SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE PREPARII I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT' ------me -----o--------- -------- -el---- - ---9-3--. 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 KSC 03-23-65 LOFC 230-390 KSC-F A 65ICD7004 - E 65ICD7006 A L C 3 9 SAT V TRANSP ROUTES -S/C 03-15-65 LOFC 230-390 KSC-EDV- D 65ICD7010 A L C 3 9 SAT V VEH STAGE 08-1 3 - 6 5 LOFC 100-390 KSC-EDV- 08-24-65 LOEL 230-390 KS C-V G-2 02-08-66 LOEL 230-390 KSC-LVO- 09-28-65 LOFC 230-390 U S C- F 65 I C D 7 0 0 3 L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G L C 3 9 OPNL T V SYS-FAC-S/C 4 S/C ESE/GSE S/C MISALIGNMENT A L C 3 9 CSM + LEM TO F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO I RN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A 65ICD7052 - S / C GSE TO HAZARD PROOF HON S Y S T l L C - 3 9 A L C 3 9 VAB H I G H B A Y AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED �. APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 5 DATE 2 9 JUL 66 -- -- --- -- D S DOC!JMENT NUMBER9 OR R E V I S I O N N O T I C E DOC REV - DOCUMENT T I T L E OR CCBD NUMBER - - -------- -------- -----a PREPARXNC I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT ' I T Y - ------------a- E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 03-18-65 COMP I N T F EI 300-230 - - MSC L V E S E / P R O P E L L A N T SYSTEMS ICD-CCBD 50 1 - 6 6 - 0 0 3 4 MSFC-ASTF L V ESE TO LAUNCH EQUIPMENT ICP-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 .-, . MSFC-ASTF SC E S E . T O L V E S E HSFC-ASTF MSFC-ASTF MSFC EDS CHECKOUT SCHEMATICS + APOLLO S C - 1 0 3 EDS DES OF SATURN S A - 5 0 4 ICD-CCBD 5 0 1 - 6 6 - 0 2 7 8 MSFC-ASTF I C D SATURN I B / V CONTROL R A T E GYRO PKG L C 3 9 S I T E P L A N + GENL ARRANGE-S/C . NO IRN-CCBD ENTERED GSE - 01-28-65 LOFC 230-390 KSC-F 02-02-65 LOFC 230-390 KSC-F ' . - .---- HSC COMP I N T E R F A C E A D E F SATURN S A - 5 0 4 APOLLO SC-103 E L E C I N T ICD-CCBD 5 0 1 - 6 6 - 0 1 4 9 - --- EDS L I M I T S A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - SCHED ACTUAL R E L D A T E REL. DATE PANEL MO D A YR MO DA YR CODE L C 3 9 DATA TRANS SYS ( W I D E BAND) NO IRN-CCBD ENTERED �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 -- --- -- .C n D S DOCUMENT NUMBER^ DOC REV S OR R E V I S I O N N O T I C E DOCUHENT T I T L E OR CCBD NUMBER --- ---------------------- ........................................ A 13H03083 R - -------- 0--9---- PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS A C T I V ------ -------------- ----- L A U VEH/SPACECRAFT PROCEDURAL R E 0 ICD-CCBD 5 0 1 - 6 5 - 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 8 10-07-65 MI 000-1 00 MSFC- L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 12-14-65 MI 000-100 HSFC- 07-07-45 HI 000-100 HS FC-I 0 SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 05-10-66 IC 000-100 MSFC - 08-17-65 IC 000-100" MSFC- 01-28-66 IC 000-100 1 - B ENVELOPE L E H / S - I V B / ICD-CC8D - A 13M65001 SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D A YR CODE I U CLEARANCE P H Y S I C A L 5 0 1-66-0099 INSTRUMENT U N I T TO SPACECRAFT PHYS REQ NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 PHYS REQ EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 L V TO S C ( C S M - 1 0 3 r L E M 4 ) I N S T R ICD-CCBD 5 0 1 - 6 6 - 0 0 7 1 IRN-CCBD 5 0 1 - 6 6 - 0 3 9 4 + COMM I N T F B D E S I G N C R I T E R I A FOR SATURN V ONBOARD EDS ICD-CCBD 50 1-66-0078 - MSFC- �AS -- --- -- DATE 29 J U L 66 D S DOCUMENT NUMBERv OR R E V I S I O N N O T I C E - .................... DOC REV 65 I C D 9 7 3 6 - 0 0 3 DOCUMENT T I T L E OR CCBO NUMBER --- SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO D A 'YR CODE ____--I- -------- PREPARING I N T E R F A C E AREAS C E N T E R OR C E I NUMBERS ACTIVITv - --------------- --I--- - - - P Y - P I P C R I T S - I C FLUSH + PURGE U N I T SAT V I C D - C C B D 5 0 1-66-0047 02-07-66 LO-FA 010-390 MSFC-EDV PHY I C D + P . I P E C R I T S I I L E A K D E T E C T SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IKN-CCBD 5 0 1 - 6 6 - 0 2 6 4 IRN-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-1 0 - 6 5 LO-FA 020-220 MSFC-EDV PHY I C D P I P E C R I T S I C FHD U M 8 SERV UN SV ICD-CCBD 5 0 1 - 6 6 - 0 1 8 0 02-10-66 LO-FA 010-220 MSFC-EDV -* SEE-DWG PHY I C D + P I P C R I T HAZ GAS A N A L Y Z E R S A T V I C D - C C B D 501-66-0100 02-04-66 LO-FA 220-000 HSFC-EDV A L C 3 9 M L PHY LOC P O R T I U WATER ACCUM CART I C D - C C B D 501-66-0207 03-02-66 LO-FA 220-390 KSC-EDV - 02-08-66 LOFC 230-390 KSC LOFC 230-390 KSC-Ef" FM 000-100 NSFC-AERO IRN-CCBD IRN-CCBD 4 80t490503 PAGE 1 5 1 CONT, SEE B A S I C NUMBER F O R R E V I S I O N o T I T L E v E T C - - 66ICD7009 ' --- ....................................... - 66 I C D 7 0 0 7 503 ...-&-- - LC-39 501-66-0377 501-66-0315 HAZARD PROOFING-S/C L C 3 9 S/C D O C o POWER S U P P L I E S F L I G H T MECHANICS PANEL I C D 01-20-66 03-09-65 I , -2 , �A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G DATE 2 9 JUL 66 AS -- --- -- 503 ----- CON?, C rt D S DOCUMENTNUMaERp OR R E V I S I O N N O T I C E __-- ------ -------------_ DOC REV IAOl PAC SCHED ACTUAL R E L DATE REL DATE P A N E L MO DA Y R HO D A YR CODE DOCUMENT T I T L E OR C C B D NUMBER -------- ___-------------__.--------------------- m------ PREP, I N T E R F A C E AREAS C E N T I OR C E I NUMBERS ACTI\ ----- --------------- - - c - c 4 9 R 2 3 65ICD9765 * R R IRN-CCBD I - f 2 * SEE B A S I C NUMBER FOR R E V I S I O N v T I T L E VE T C . J 65ICD9770 - J 651CD9771 - 1 V PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 7 - R PHY I C D H E A T EXCHANGER A 7 - 7 l / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 - - * 501-66-0300 PNEU S Y S / S A T U R N V 06-25-65 LO-FA 220-390 KSC-F 0 2 - 1 1-66 LO-FA 220-390 HSFC- SEE-DUG P H Y S I C D S - I C H Y D R A U L I C U N I T LC39 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 02-10-66 LO-FA 220-390 KSC-X PHY I C D S - I C PNEU CONSOLE RKS 1 - 2 - 3 + 4 I C D - C C B D 501-65-61 09-1 5-65 LO-FA 220-390 KSC-X 08-09-65 LO-FA 220-390 KSC-P PHY I C D S - I C PNEU CHECKOUT RKS 1 - 2 - 3 + 4 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 HSFC- P I P I N G CRITERIA S-IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 220-280 12-09-65 LO-FA 210-390 PHY I C D PNEU CONSOLES 5 1 6 . 7 ICD-CCBD 5 0 1 - 6 5 - 3 4 + 8 S-IC PNEU CONSOLE S E T A S - I I STAGE G S E P L A C E H E N ? ON HBL LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 - HSFC- KSC-E �. APOLLO 1NTERFAC.E CONTROL DOCUMENT LOG PAGE 14' D A T E 29 J U L 66 --- -- --- -- D DOCCMENT NUMBER, OR REVISION NOTICE _ _S .................... DOC REV -0- SCHED ACTUAL REL DATE R E L . D A T E PANEL MO DA YR M O DA YR CODE DOCUMENT TITLE OR C C B D NUMBER ........................................ PREPARING INTERFACE AREAS CENTER OR CEI NUMBERS ACT ' T Y -------- -------- ------ -------------- --------- ICD-CCBD 50 1-66-0106 J 65ICD9757 R - PHY ICD IU COOLING UNIT + PIPING CRIT ICD-CCBD 50 1-65-49 IRN-CCBD 501-66-0376 09-15-65 LO-FA 220-390 MSFC-EDV - PHY ICD IU PNEU CONS + PIPING CRITERIA ICD-CCBD 50 1-65-48 IRN-CCBD 501-66-0292 09-1 5-65 LO-FA 220-390 MSFC-EDV 06-21-65 LO-FA 220-390 KSC-P+VE PHY ICD S-IC INERT PREFILL + PIPING CRXT ICD-CCBD 501-65-47 09-15-65 LO-FA 220-390 MSFC-EDV PHY ICD S-I1 PNEU CONSOLES S7-41B/SAT V ICD-CCBD 501-65-28 IRN-CCBD 501-66-0124 IRN-CCBD 501-66-0301 06-25-65 LO-FA 220-390 KSC-P+VE PHY ICD SII P N E U CONSOLE S7-41C/SAT V ICD-CCBD 501-65-29 IRN-CCBD 501-66-0128 IRN-CCBD 501-66-0294 06-25-65 LO-FA PHY ICD SII PNEU CONS S7-41A+41D/SAT V ICD-CCBD 501-65-30 IRN-CCBD 501-66-0130 06-25-65 LO-FA 2 - PHY ICD APS PNEU C O N S DSV-40-436/SAT ICD-CCBD 501-66-0104 V PIPING- CRITERIA APS PNEU CONSOLE LC39 IRN-CCBD 501-66-0314 t �IAOP APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE D A T E 2 9 J U L 66 -- --- -SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR HO DA YR CODE C ti " DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV -------- -------- ------ ------------- DOCUMENT T I T L E OR CCBD NUMBER ___ - -------------------- --- ........................................ IRN-CCBD - - PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I ------ 501-66-0126 U M B I L I C A L 4 S E R V I C E CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - O L 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED UMB 4 SERV CONNECTIONS S - I V B ICD-CCBD 501-66-0178 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 8 FORWARD AFT UMB + S E R V I C E CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 3 FORWARD U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 s IRN-CCBD 5 0 1 - 6 6 - 0 2 8 4 06-28-65 LO-FA 020-390 KSC-P+\ 06-21-55 LO-FA 040-390 KSC-P+\ 06-1 8 - 6 5 LO-FA 040-390 KSC-P+\ 06-1 8 - 6 5 LO-FA 090-390 KSC-P+l PHY I C D S - I V B PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 V 06-21-65 LO-FA 220-390 KSC-K-I PHY I C D S - I V B PNEU CONS O S V - 4 8 - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 , V 06-21-65 LO-FA 220-390 KSC-P+' PNEU CONS SET L C 3 9 01-28-66 LO-FA 020-390 KSC-P+\ 06-21-65 LO-FA 220-390 . KSC-P+\ PIPING CRITERIA S-IVB ICD-CCBD 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 9 PHY I C D S - I V B H T EXCH D S V - 4 8 - 4 3 8 / S A T Y �:t @ S ,- - 7.. 2LS -- J U L 66 --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E .................... SCHED ,'ICTfJAI.. R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ....................................... IRN-CCBD IRN-CCBD - - 5 0 1-66-0282 501-66-0382 M O T I O N ENV A F T UMB P L A T E S 1 9 2 9 + 3 S - I C ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-10-65 LO-FA PHY I C D L A U VEH S - I C 160-CCBD 5 0 1 - 6 5 - 3 6 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 6 IRFI-CCBD 5 0 1 - 6 6 - 0 3 7 8 I N T K UMB/LC39 08-09-65 LO-FA PHY I C D L A U VEH 5 - I C FWD U M B / L C 3 9 GSE 08-09-55 LO-FA 06-28-65 LO-FA - U M B I L I C A L + SERV CONN S I I L O X DISCONNECT ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 . IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-21-65 LO-FA - - U M B I L I C A L + SERV CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 06-21-65 LO-FA UMB + SERV CONNECTIONS S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CC8D 5 0 1 - 6 6 - 0 3 8 3 GSE INTERM LH2 DISC - -------- -------- ------ -------------- --------- ICD-CCBD 5 0 1 - 6 5 - 3 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO IRN-CCBD ENTERED - P R c 0 6 P Ir!C I N T E R F A C E AREAS CEN""9 OR C E I N U M B E R S AC1 ITY �. APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl PAGE D A T k 2 9 J U L 66 -- --- -- .* i DOCUMENT NUMBER, OR R E V I S I O N N O T I C E SCHED ACTUAL R E L D A T E R E L DATE P A N E L HO DA YR MO D A YR CODE DOC REV DOCUMENT T I T L E OR CCBD NUMBER ___ _ .................... --- ....................................... ; s S R A 65ICD9405 R R IRN-CCBD 4 I - 1 2 - FUNCT I N T F F L U I D REQMTS RP-1 ICD-??O)'3 5 0 1 - 6 6 - 0 0 4 1 -- I 1 2- - - * > * A -I-" j.? i Cfi-,,I;EiQ IRN-CCeD IRN-CCBD ; '0 1 : , -- ii. ;> {,, ! :j-{,! .. . 1 ,;" :;IC 4FT .. I! , .> .< ): ,,,L. ? 1.;'' . , .+. . . . .-: .' 1- ... .-:-:. ..> :. -. , .lL- ....-.. . ' ... AFT .. :-( "4 . , .. ', ...,;,. . L "., I . I -,L ~ ~ ;'.i-ril'E I NU 1-2 S-IC --. ,. - -, - :. . -. .. -,,, , ., k: c, i : . ; : : . . . d - ~ . - y i ~ ! , t -. 9.-. ------c -c---- 06-03-65 LOPG 010-250 KSC-P+V 06-15-65 LOPG 010-250 KSC-P+V 08-20-55 LO-FA (3 ID-.; 1 fl ESC-P+V ., 5 t r : i l t:ilY?.l P l ATE 3-4 <,'I'- --o-,--.'+;.i 1 ii!l'lh -r;\iJ:) SYS SAT V 501-66-0299 5 0 1-66-0289 L ~ N - L C ~ 531-66-0378 U - -------------- --Ds---- 501-66-0318 FUNCT I N T F F L U I D REQMTS LOX SYS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1-66-0040 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 .. - -------- PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT . -... : . * . , I .,T< 141.1 :I-,: li-1.C AFT �PAGE DATE 2 9 J U L 6 6 -- --- -- .- u -S DOCUMENT NUMBER^ OR R E V I S I O N NOTICE -----------e------- DOC REV ACTUAL SCHED R E L D A T E RE( D A T E PANEL MO DA Y R MO DA YR CODE -l -l PREPAR IN( -------- -------- ------ -------------- --------- DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ INTERFACE A R E A S C E N ~ F R OR C E I NUMBERS AC.. TTY ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED A 65ICD9205 - - L V E S E TO KSC DATA MEASUREMENTS 02-11-66 LOEL 220-290 MSFC-ASTI LOW BAY ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-1 1 - 6 6 LO-EL 220-290 MS F C LOW BAY ESE TO I N S T R SYS AND REC ICD-CC8D 5 0 1 - 6 6 - 0 0 8 2 02-11-66 LO-EL 220-290 MSFC-ASTI S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRM-CCBD 50 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSFC-KSC FUNCT I N T F F L U I D REQMTS GHE SYS S A T V 06-28-65 LOPG 010-250 KSC-P+VE 06-28-65 LOPG 010-250 KSC-P+VE 06-28-65 LOPG 010-250 KSC-P+VE 06-28-65 LOPG 010-250 KSC-P+VE NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - f ENTERED ENTERED ENTERED FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED FUNCT I N T F F L U I D REQMTS GH2 SYS S A T ' V ' NO IRN-CC8D ENTERED . - ' , - FUNCT I N T F F L U I D REQMTS L H 2 S Y S SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 JUL 6 6 : r DOCUMENT NUMBER, OR R E V I S I O N NOTICE AS DOC REV 503 CONTo __ _ _---------------------- ------------------------------------- ; S DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD E 65ICD9080 - - - - SCHED ACTUAL REL DATE REL D A T E PANEL HO DA YR MO D A YR CODE ---04--- -lo----- PREPARI! I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y - -----a 50 1-66-0086 LC39 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSG-EDV- L C - 3 9 PAD AREA L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EDV- S - I C / M L HOLD DOWN ARMS P H Y S I C A L REQHTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC LOFC 000-040 HSFC LO-EL 220-390 HSFC-AS- 220-390 MSFC-AS? WIND LOAD A L L E V I A T I O N S Y S F A C I L TO L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E E S E ICB-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - PAGE 09-01-66 03-09-66 L V E S E TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBP 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 02-11-66 LO-EL L V ESE TO I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRM-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL HSFC COUNT CLOCK T O KSC T I M I N G L C - 3 9 �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE L DATE 29 J U L 6 6 D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E -- - ------------------E 65ICD8002 A 65ICD8200 J 651CD8300 R 1 R 2 - DOC REV DOCUMENT T I T L E OR CCBD NUMBER ...................................... A S/C - A.Ce POWER REC. FUNCT I N T F REQMTS ECS MC LEM S / C GSE LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD B L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD J 651CD8302 - - LC34/37/39 - PREPARIN ?R INTERFACE AREAS C F OR C E I NUMBERS A C i r V I T Y -------- -------- ------ --------------- -------11-29-65 LOFC 230-347 KSC-EDV- 05-03-65 LOPG 230-300 KSC-K-DT 230-340 KSC-EDV 230-340 KSC-D 230-300 MSC-FO SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED SWG ARM UM8 D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED C M D MOD ACCESS ARM CABLING VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP - + CONN SCHED ACTUAL R E 1 D A T E R E L DATE P A N E L MtJ DA YR MO DA YR CODE t 23 AFRM 9 T O ACCESS ARM WHT RM 03-17-65 LOFA 230-300 KSC-DE C / M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 MSC-EDV PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 501-66-0164 COVER 12-10-65 LO-FA 110-300 KSL-EDV SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC L C 3 9 VAB H I G H BAYS TO L / V 11-19-65 LOFC 220-390 KSC-F 02-09-66 LO-FC 220-390 KSC-EDV-; ESE/GSE LC 3 9 V A B LOW BAY AREA TO L/V-ESE/GSE �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G PAGE DATE 2 9 J U L 66 -- --- -- C W c ___ D _ DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV --- DOCUMENT T I T L E OR CCBD NUMBER --------^-C NO NO NO NO NO NO NO NO NO NO J 651CD7788 LC39-LUT - a ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED - A 65ICD8001 IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTTVI' -------- -------- ------ -------------- -P-CIPY-li--C.----OQ-l.-i.------ L C 3 9 A ML P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NU IRN-CCBD ENTERED NO IRN-CCBD ENTERED - + .--- - - SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO D A YR CODE F L SYS 11-17-64 LOFA 230-390 KSC-DE 07-22-65 LOFA 230-390 KSC-EDL LEM U M S I L I C A L AND T E S T CABLES FOR L C 3 9 NO IRN-CCBD ENTERED 08-20-65 LOFA 230-390 + 09-22-64 LO-FC 230-340 GSE CABLES-GAS N I T SYS L C 3 9 PHY I N T F C GOX CON0 PNL L E A K TS U N I T NO IRN-CCBD ENTERED ACCESS ARM NO TRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD + SERV MODULE CABLE REQMTS ENTERED ENTERED ENTERED ENTERED \ LC/34/37/39 TIMING COUNTDOWN D I S T KSC-EDV �APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE 1 4 DATE 2 9 JUL 6 6 -- --- -- D S ,- DOC!jMENT NUMBER9 OR R C V I S I O N NOTICE -- DOC REV - -------------------- --- - F 65ICD7468 - DOCUMENT T I T L E OR CCBO NUMBER SCHED ACTUAL REL DATE R E t DATE PANEL MO DA YR PI0 D A YR CODE -------- -------- PREPARINC INTERFACE AREAS CENTER OR CEI N U M B E R S ACT"'1TY ----- -------------- --- ---- ------------------------------I-------- NO IRN-CCBD NO 1 RN-CCBD ENTERED ENTERED L C 3 9 PIPI.NG NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD C R I T + I N T F LOC S / C F L D SYS ENTERED ENTERED ENTERED ENTERED LC39/MSS P I P C R I T + I N T F L O C LEM F L D SYS L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD 09-03-65 LOPG 12-02-65 LOPG KSC-EDV 01-12-65 LOFC KSC-F 03-19-65 LOPG KSC-K-DT 100-200 KSC ENTERED ENTERED FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO IRN-CCBD ENTERED FUNCT I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG KSC-EDV FUNCT I N T F REQMTS G N 2 L C 3 9 A S/C GSE 05-02-66 LOPG KSC-K-DT 02-09-66 LOPG KSC-EDV 02-10-66 L/-FC KSL FUNCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE 03-19-65 LOPG KSC-K-DT L C 3 9 LUT GSE SYSTEMS APRM CONFIG NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 11-05-64 LO-FC MSC-NAA L C 3 9 A S / C GSE FUNC I N T F REQtGOX LC-39 PAD 0 S / C �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 PAGE 1 -- --- -- f , 5 DOCUMENT NUMBER9 OK R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER _- - -------------------- --- ........................................ NO NO NO NO NO NO NO NO NO NO A 65ICD7166 A 65ICD7167 - IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA YR CODE PREPAR IP I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T ) ----I--- ---o---------- -------- ------ - -------- ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED FUNCT I N T F REQS ECS L C 3 9 V A B S/C-GSE FUNCT I N T F RQMTS ECS L C 3 9 1 V A B LEM SC L C 3 9 LCC F A C I L I T Y S / C ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED GSE ., 03-19-65 LOPG 100-390 KSC-K-Dl 05-03-65 LOPG - 230-390 KSC-K-Dl 230-390 KSC-F 230-390 KSC-F 03-05-65 01-25-65 , , LOFC �P A G E 13 DATE 2 9 J U L 66 -- -- --- -- D S DOCllMENTNUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER - - -------------------- --- -__------------------------------------ L C 3 9 DATA TRANS S Y S ( W 1 D E BAND) NO IRN-CCBD SCHED ACTUAL R E 1 D A T E R E L DATE P A N E L MO DA YR MO bA YR CODE -------- -------- ------ PREPARING I N T E R F A C E AREAS CENTER OR CEI NUMBERS A C T Y V I T Y ---- P----I-- 02-02-65 LOFC 230-390 KSC-F 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 KSC 03-23-65 LOFC 230-390 KSC-F ENTERED 6 5 1CD7003 - L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G A 65ICD7004 - L C 3 9 OPNL T V SYS-FAC-S/C E 65ICD7006 A L C 3 9 S A T V TRANSP ROUTES -S/C 03-1 5 - 6 5 LOFC 230-390 KSC-EDV-2 D 65ICD7010 A L C 3 9 S A T V VEH STAGE + S / C M I S A L I G N M E N T 08-13-65 LOFC 100-390 KSC-EDV-2 A L C 3 9 CSM + LEM T O F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRM-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 08-24-65 LOEL 230-390 KSC-VG-2 230-390 KS.6-LVO-; 230-390 KSC-F A 65ICD7002 A 65ICD7052 - L C 3 9 OPNL INTERCOM SYS-S/C S/C ESE/GSE S/C ESE/GSE GSE TO HAZARD PROOF MON S Y S T v L C - 3 9 A L C 3 9 V A B H I G H BAY AREA TO S / C NO IRN-CCBD ENTERED 04-28-65 LOFC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 DATE 29 J U L 6 6 -- --- -- D S DOCUMENT NUMBERo 3 R R E V I S I O N NOTICE - DOC REV ._- ____------------------ SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA Y R MO D A YR CODE DOCUMENT T I T L E OR CCBD NUMBER A 16331-63A107350 A 16331-63A107393 - C-S 000-100 MSFC 08-06-65 C-S 000-100 MS FC-AS1 03-18-65 E I 300-230 MSC 08-12-65 EJ 300-100 MSC L V E S E / P R O P E L L A N T SYSTEMS XCD-CCBD 5 0 1 - 6 6 - 0 0 3 4 12-15-65 €1 220-210 MSFC-AST L V ESE TO LAUNCH EQUIPMENT ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1-66-0189 12-09-65 EX 220-210 MSFC-AST I+ A 401.105496 E I 220-230 MS FC-AST EI 000-100. - A t+ rJM37543 EI 000-220 CS 000-100 MSFC-AST, A 50M36801 H- NF 040-090 MSFC-M-El LOFC 230-390 KSG-F 07-01-67 EDS L I M I T S E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 COMP I N T F A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - - - --O-------U------UO--------------------- B D E S I G N C R I T E R I A FOR SATURN V ONBOARD EDS ICD-CCBD 5 0 1 - 6 6 - 0 0 7 8 A 13M65503 PREPAR I N I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY COMP I N T E R F A C E SC E S E TO t V E S E 06-01-66 DEF OF S A - 5 0 3 APOLLO S C - 1 0 2 ICD-CCBD 5 0 1 - 6 6 - 0 0 6 9 ELEC I N T F 04-05-65 EDS CHEC.KOUT SCHEMATICS DES OF SATURN SA 5 0 3 ICD-CCBD 5 0 1 - 6 6 - 0 2 8 0 + 03-30-67 APOLLO S C - 1 0 2 I C D SATURN I B / V CONTROL RATE GYRO PKG L C 3 9 S I T E P L A N + GENL,ARRANGE-S/C NO IRN-CCBD ENTERED GSE EDS 03-11-66 03- 15-66 01-28-65 , . MSFC-AST MSFC - �. APOLLO I N T E R F A C E CONTROL DOCUMENT L O G P A G E 13 DATE 2 9 J U L 66 -- -- --- -- DOC!JMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ - L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD IRN-CCBD 13M07083 - 501-65-77 501-66-0198 L A U V E H I S P A C E C R A F T F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 B ENVELOPE L E M / S - I V B / I U CLEARANCE P H Y S I C A L ICD-CCBD 5 0 1 - 6 6 - 0 0 9 9 - - INSTRUMENT U N I T T O SPACECRAFT PHYS REQ ICD-CCBD 5 0 1 - 6 6 - 0 1 0 1 IUtI-CC8D 5 0 1 - 6 6 - 0 1 0 1 IRN-CC8D 5 0 1 - 6 5 - 0 1 0 1 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 PHYS REP B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 L V TO S C ( C S M - 1 0 2 r L E M - 3 ) I N S T R ICD-CCBD 5 0 1 - 6 6 - 0 0 7 2 IRN-CCBD 5 0 1-66-0396 + COMM I N T F SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO D A YR CODE PREPARING ----- I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T - . I T Y -------- -------- ------ -------------- s-- �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG D A T E 29 JUL 66 - -- --- -- PAGE " I? r u DOCUMENT NUMBERo OR R E V I S I O N NOTICE DOC REV 6 5 ICD9776-003 DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE -------- -------- PHY I C D P I P E C R I T S I C FWD UMB SERV UN SV ICD-CCBD 5 0 1 - 6 6 - 0 1 8 0 0 2 - 1 0-66 -r=---- LO-F A SEE B A S I C NUMBER FOR R E V I S I O N p T I T L E , E T C o 1 - PHY I C D ICD-CCBD IRN-CCBD IRN-CCBD PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT --------------010-220 s------ MSFC-ED' SEE-DWG + P I P C R I T HAZ GAS ANALYZER SATV 02-04-66 LO-FA 220-000 MSFC-ED\ 03-02-66 LO-FA 220-390 KSC-EDV 02-08-66 LOFC 230-390 KSC LOFC 230-390 KSC-EDV- 501-66-0100 501-66-0377 501-66-0315 A L C 3 9 M L PHY LOC PORT I U HATER ACCUM CART ICD-CCBD 5 0 1 - 6 6 - 0 2 0 7 - LC-39 - LC39 S / C DOC, POWER S U P P L I E S HAZARD PROOF1 NG-S/C A I R N NO 2 TO FMP I C D NO IRN-CCBD ENTERED 0 1-2 0-66 - �. APOLLO I N T E R F A C E CONTROL DOCUMENT LUG DATE 2 9 J U L 6 6 AS -- --- -- D __ S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV .................... --- + - - - --. SCHED ACTUAL REL DATE R E L . DATE PANEL MO D A Y R MO DA YR CODE -_-------------- ---I------------------------------------ o----- PREPARING --------------- --- ---I N T E R F A C E AREAS C E N T E R OR C E I NUMBERS A C T T " I T Y 5 0 1-66-0045 501-66-0327 SEE BAS! C NUMBER FOR R E V I S I O N o T I T L E , E T C - SEE-D#G PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCSD 5 0 1 - 6 6 - 0 1 8 3 02-10-66 LO-FA 220-390 KSC-K-DT PHY I C D S - I C PNEU CONSOLE RKS 1-2-3+4 ICD-CCBD 501-65-61 09-1 5-65 LO-FA 220-390 KSC-K-DT PHY I C D PNEU CONSOLES 5 ~ 6 . 7 + 8 S - I C ICD-CCBD 5 0 1 - 6 5 - 3 4 08-09-65 LO-FA 220-390 KSC-P+VE 09-24-65 LO-FA 220-390 HSFC-EZV 02-07-66 LO-FA 220-280 HSFC-P+V i 12-09-65 LO-FA 210-390 KSC-EDV P I P C R I T S - I C F L U S H + PURGE U N I T SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 7 02-07-66 LO-FA 010-390 HSFC-EDV PHY I C D + P I P E C R I T S I ' I L E A K DETECT SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 4 IRN-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-10-65 LO-FA 020-220 MS-FC-EW PHY I C D S - I C PNEU CHECKOUT RKS 1-2-3*4 ICD-CCBD 5 0 1-65-46 P I P I N G CRITERIA S-IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 6 IRN-CCBD 50 1-66-0306 ; PNEU CONSOLE SET A S - I I STAGE GSE PLACEMENT ON MBL LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 - P A G E i3! CONT. DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD 65 ICD9766-003 502 ----- c �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE I DATE 2 9 J U L 6 6 - -- --- -- D S DOCUMENT NUMBERo 3R R E V I S I O N N O T I C E R DOC REV 1 - J 65ICD9760 - R DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD J 65ICD9759 1 - - - SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE -------- ------- ------ PREPARIb I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY - -------------o- -------- 501-66-0292 06-22-65 LO-FA 220-390 KSC-P+VE P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 501-66-0314 02-10-66 LOFA 220-390 MS FC-EDU PHY I C D S - I C I N E R T P R E F I L L ICD-CCBD 5 0 1 - 6 5 - 4 7 09-15-65 LO-FA 220-390 MSFC-EDV 06-2 5-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE PHY I C D APS PNEU CONS D S V - 4 0 - 4 3 6 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 9 V PIPING CRIT PHY I C D S - I 1 PNEU CONSOLES S 7 - 4 1 B / S A T ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 PHY I C D S I I PNEU CONSOLE S 7 - 4 1 C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 1 D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S-I1 V V V V PNEU S Y S I S A T U R N V 06-25-65 LO-FA 02-11-66 LO-FA , .. .- +, 220-390 KSC-P+VE 220-390 MSFC-EDV . . . �9 APOLLO I N T E R F A C E CONTROL DOCUMENT L O G PAGE 1: DATE 2 9 - J U L 66 -- -- --- -- .- D S DOClJMENT NUHBERI OR R E V I S I O N N O T I C E - .................... DOC REV SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA Y R MO DA YR CODE DOCUMENT T l T L E OR CCBD NUMBER --_ ........................................ ICD-CCBD IRN-CCBD IRN-CCBD - - - - -------- ------- ------ ------------ --------- 501-66-0178 5 0 1-66-028 1 501-66-0288 UMB + S E R V I C E CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 3 FORWARD U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 IRM-CCBD 5 0 1 - 6 6 - 0 2 8 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 4 PHY I C D S - I V B PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 501-66-0107 V PHY I C D S - I V B PNEU CONS DSV-4B-433/SAT ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V P I P I N G CRITERIA S-IVB ICD-CCBO 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 4 PNEU CONS SET L C 3 9 PHY I C D S - I V B H T EXCH D S V - 4 B - 4 3 8 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 6 V PHY I C D I U C O O L I N G U N I T + P I P I N G C R l T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 - PHY PREPARIN( I N T E R F A C E AREAS CENTER OR C E I NUMBERS AC" ITY I C D XU PNEU CONS + P I P I N G C R I T E R I A ICD-CCBD 5 0 1 - 6 5 - 4 8 . 06-18-65 LO-FA 040-390 KSC-P+VE 06-1 8 - 6 5 LO-FA 090-390 KSC-P+VE 06-21-65 LO-FA 220-390 KSC-K-ST 06-21-65 LO-FA 220-390 KSC-P+VE 01-28-66 LO-FA 020-390 KSC-P+VE 06-21-65 LO-FA 220-390 KS' 09-15-65 LO-FA 220-390 MSFC-EDV 09-1 5 - 6 5 LO-FA 220-390 PISFC-EDV +VE - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 C AS DOCUMENT NUMBER? OR R E V I S I O N N O T I C E DOC REV 502 CONTO __ _ .................... --- ---------------------------------------S IAOl DOCUMENT T I T L E OR CCBD NUMBER PAGE 9, SCHED ACTUAL R E L D A T E R E L DATE PANEL MO D A YR MO DA YR CODE -------- -------- ------ PREPAR I h I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVITY - -------- ---o---------- ICD-CCBD 5 0 1 - 6 5 - 3 6 IRN-CCBD~ 501-66-0290 IRM-CCBD 5 0 1 - 6 6 - 0 2 9 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 I - PHY I C D L A U VEH S - I C FWD U M B / L C 3 9 GSE 08-09-65 LO-FA 010-390 KSC-P+VE 06-28-65 LO-FA 020-390 KSC-P+VE ICD-CCBD 5 0 1 - 6 5 - 3 7 IRN-CCBD 5 0 1-66-0190 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO IRN-CCBD ENTERED - - - UMB + SERV CONNECTIONS S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 501-66-0383 INTERM . .- U M B I L I C A L 9 SERV CONN S I I LOX DISCONNECT ICD-CCBO 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-21-65 LO-FA 020-390 KSC-P+VE UMBILICAL SERV CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 6 06-21-65 LO-FA 020-390 KSC-P+VE 06-28-65 LO-FA 020-390 KSE-P+VE 06-21-65 LO-FA 040-390 LH2 DISC U M B I L I C A L + S E R V I C E CONN S - , I I ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED , FORWARD . KSC-P+VE �APOLLO INTERFACE AS- DATE 2 9 J U L 66 -- --- -- D S DOCUMENTNUMBERt 3R R E V I S I O N N O T l C E CONTROL DOCUMENT LOG 502 1 A01 PAGE 1 CONTO - -----. SCHED ACTUAL R E L D A T E REL DATE PANEL MO DA YR MO D A YR CODE DOC REV DOCUMENT T I T L E OR CCBD NUMBER -- - ------------------- --- ....................................... - FUNCT I N T F F L U I D REQMTS R P - 1 SYS SAT PREPAQ I N I N T E R F A C E AREAS CEFt'EFI OR C E I NUMBERS AC JITY -------- -------- ------ ------------- -------- 06-1 5-65 LOPG 010-250 KSC-P+Vf FUNCT I N T F F L U I D REQMTS V A B ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED 05-1 9-65 LOPG 000-260 KSC-K-DT P I P C R I T APS PROP S E R V I C I N G SAT V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-EDV UKB AND SERV CONN P L A T E 3-4 ICD-CCBD 5 0 1 - 6 5 - 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 08-10-65 LO-FA V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CCBD. 5 0 1 - 6 6 - 0 0 4 1 - - - J 65IC09744 - S I C AFT UMB + SERV CONNS P L A T E NO 1-2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT 08-18-65 LO-FA UMB + SERV CONNS P L A T E NO 3-2 ICD-CCBD 5 0 1 - 6 5 - 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT 08-10-65 LO-FA 08-10-65 LO-FA 08-09-65 LO-FA H O T I O N ENV A F T UMB P L A T E S 1 , 2 9 + 3 ICD-CCBD 5 0 1-66-0042 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 PHY I C D L A U VEH S - I C S-IC I N T K U M B / L C 3 9 GSE , 010-21 0 MS. ,-P+V �, APOLLO INTERFACE CONTROL DOCUMENT LOG AS DATE 2 9 J U L 6 6 -- --- -- 502 ----- Y H ___ _ C J DGCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV - - PAGE SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO DA YR CODE PREPARI INTERFACE AREAS CENTER OR C E I NUMBERS A C T X V I T ------. LOW BAY ESE TO I N S T R SYS AND REC ICD-CCBD 5 0 1 - 6 6 - 0 0 8 2 02-11-66 LO-EL 220-290 MSFC-AS S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 HSFC-KSl FUNCT I N T F F L U I D REQMTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+V' FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VI FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VI FUNCT I N T F F L U I D REQMTS L H 2 SYS SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 , 06-28-65 LOPG 010-250 KSC-P+VI FUNCT I N T F F L U I D REQMTS LOX SYS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CC8D 5 0 1 - 6 6 - 0 0 4 0 06-03-65 ICD-CCBD I CONT. -------- ------ -------------- DOCUMENT T I T L E OR CCBD NUMBER _-_____-------------- ........................................ A 65ICD9241 IAOl ---4---- 501-66-0171 ' LOPG 010-250 KSC-P+VE �. APOLLO 1NTERFAC.E CONTROL DOCUMENT LOG DATE 29 JUL -- --- .D 66 - AS .. DOCllHENT NUMBER9 OK R E V I S I O N N O T I C E . 502 ----- DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -S ------------------- --- ...................................... - --. SCHED ACTUAL R E L D A T E R E L . D A T E PANEL MO DA YR MO D A YR CODE PREPARING I N T E R F A C E AREAS CENTER OR CEI NUMBERS ACT :TY - LO-FC 220-390 HSFC LOFC 000-040 MS FC 03-09-66 LO-EL 220-390 MSFC-ASTR L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 50 1 - 6 6 - 0 1 7 4 I~N-CCBD 501-66-0324 02-11-66 LO-EL 220-370 MSFC-ASTR LV ESE TO I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 50 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL 220-290 MSFC COUNT CLOCK T O KSC T I M I N G L C - 3 9 ICD-CCBD 50 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED 08-14-65 LOEL 200-390 - L V ESE TO K S C DATA MEASUREMENTS 02-11-66 LOEL 220-290 MSFC-ASTR .- LOW B A Y ESE TO I N S T R U SYS + REC 02-1 1-66 LO-EL 220-290 NSFC - - - 04-05-66 S - I C f M L HOLD DOWN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 WIND LOAD A L L E V I A T I O N S Y S F A C I L T O L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E ESE ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - PAGE 12' CONTa 09-01-66 L V ESE TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 t . HSFC-ASTR MSFC-ASTR - �A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G IA 0 1 . DATE 2 9 JUL 66 -- --- -- C u DOCUMENT NUMBER, DOC G OR R E V I S I O N N O T I C E REV DOCUMENT T I T L E OR CCBO NUMBER SCHED ACTUAL R E L DATE R E L DATE PANEL MO D A Y 8 MO D A YR CODE --mb--- NO I R N - C C S D NO I R N - C C B D a B L C 3 7 / 3 9 LEM NO I R N - C C B D NO I R N - C C B D NO I R N - C C B D - LC34/37/39 - - - - ?REPAR I N T E R F A C E AREAS CENTER OR C E I MUNBERS ACTIVf' --------------- ------. I * . . . - ENTERED ENTERED SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED CMD MOD ACCESS ARM C A B L I N G V E R T STOP F O R L E S A C C E S S ARM NO IRN-CCBD E N T E R E D NO I R N - C C B D E N T E R E D A HOCK-UP ------- PAGE 23 A F R M 9 T O ACCESS ARM WHT RM 11-17-64 LOFA 230-340 KSC-D 11-18-64 LOFA 230-300 HSC-FO 03-17-65 LOFA 230-300 KSC-DE C / M ACCESS ARM ADPT HOOD T O S / C XNTF REQ 11-04-65 LOFA 100-300 HSC-ED\ P H Y l NTF R E T R A C T I O N MECH Q-BALL I C D - C C B D 501-66-0164 COVER 12-10-65 LO-FA 110-300 KSC-ED\ S A T U R N V L A U N C H V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC 220-390 L C 3 9 VAB H I G H BAYS TO L I V ESE/GSE 11-19-65 LOFC 220-390 LC 3 9 V A B LOW B A Y A R E A T O L / V - E S E / G S E I C D - C C B D 501-66-0086 02-09-66 LO-FC 220-390 -K S C - E D i L C 3 9 MSS TO L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-EDC LC-39 12-07-65 LOFC 220-390 KSC-EDY - MSFC KSC-F . PAD AREA L / V ESE/GSE �. APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 29 J U L 6 6 -- --- -- D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E - - .................... DOC REV --- DOCUMENT T I T L E OR CCBD NUMBER - - ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED L C 3 9 A ML P I P C R I T + I N T F L O C S/C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED F L SYS 08-20-65 LOFA 230-390 KSC-EDV 11-17-64 LOFA 230-390 KSC-DE L C 3 9 PHY I N T F C GOX COND PNL LEAK TS U N I T NO IRN-CCBD ENTERED 07-22-65 LOFA 230-390 KSC-EDV ACCESS ARM + SERV MODULE CABLE REQMTS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 09-22-65 LOFA 230-390 KSC-EDV LEM U M B I L I C A L AND T E S T CABLES FOR L C 39 NO IRN-CCBD ENTERED 08-20-65 LOFA 230-390 KSC -DV 09-22-64 LO-FC 230-340 11-29-65 LOFC 230-347 KSC-EDV-2 05-03-65 LOPG 230-300 KSC-K-OT LC39-LUT GSE CABLES-GAS LC/34/37/39 A S/C - IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD PREPARINC INTERFACE AREAS CENTcR OR C E I NUMBERS A C i iTY -------- -------- ------ --------------- --------_ ---------------------------s---s--s-- NO NO NO NO NO NO - SCHED ACTUAL R E 1 DATE REL' DATE PANEL MO DA YR MO DA YR CODE A.C, N I T SYS T I M I N G + COUNTDOWN D l S T POWER REC. 4 CONN FUNCT I N T F REQMTS ECS MC LEM S/C LC 3 4 / 3 7 / 3 9 , GSE SM SWG ARM U M 0 D I S C A 1 4 0 1 9 , - �, APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 J U L 66 AS -- --- -- 502 ----- CON?. PAGE 8 C n S S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER NO NO NO NO - IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVI ------- -------- ------ ------------ ----0- ENTERED ENTERED ENTERED ENTERED P I P C R I T + I N T F LOC LEM F L D SY.S 12-02-65 LOPG 140-390 KSC-ED\ 01-12-65 LOFC 230-390 KSC-F FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO, IRN-CCBD ENTERED 03-19-65 LOPG FUNCT I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-ED' FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-K-I - L C 3 9 A S / C GSE FUNC I N T F REQvGOX 02-09-66 LOPG 230-390 KSC-ED' - LC39 LOFC 230-330 KSC-F - FUNCT. I N T F REQS ECS L C 3 9 PAD 8 S/C-GSE 03-19-65 LOPG 100-390 KSC-K- 11-0 5-64 LO-FC 230-390 - - - LC39/MSS L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - ENTERED ENTERED ENTERED PAD B 0 L C 3 9 L U T GSE SYSTEMS AFRH C O N F I G NO I RN-CCBD E N T E R E D . NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-01-66 a MSC-NA �A P O L L O I N T E R F A C E C O N T R O L DOCUMENT L O G iA01 PAGE 1 2 5 D A T E 2 9 J U L 66 -- --- -- D S DOCUMENTNUMBER* OR REVISION NOTICE --- DOC REV DOCUMENT T I T L E O R C C B D NUMBER SCHED ACTUAL R E L DATE R E L DATE PANEL MU DA YR MO D A YR C O D E ---PO--- PREPARING I N T E R F A C E AREAS C E N T E ACTIVITY OR C E I NUMBERS ------- ------ -------------- ---------4 NO NO NO NO NO NO IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD NO I R N - C C B D NO I R N - C C B D NO I R N - C C B D - - ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED FUNCT I N T F REQS E C S L C 3 9 VAB S/C-GSE 03-1 9-65 LOPG 100-390 KSC-K-DT F U N C T I N T F RQMTS E C S L C 3 9 / V A B LEM S C G S E 05-03-65 LOPG 230-390 KSC-K-DT L C 3 9 LCC F A C I L I T Y S / C E S E / G S E NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E O 03-05-65 230-390 KSC-F A L C 3 9 MAT-ESE/GSE NO I R N - C C B D E N T E R E D NO I RN-CCBD E N T E R E O NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO IRN-CCBD E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO IRN-CCBD E N T E R E D - L C 3 9 P I P I N G C R I T + I N T F L O C S/C F L D S Y S - 01-25-65 LOFC 230-390 KSC-F 09-03-65 LOPG 100-200 KSC �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl D A T E 29 JUL 66 PAGE -- --- -- -* D 7 DOCUMENT N U M B E R , OR R E V I S I O N N O T I C E DOC REV SCHED ACTUAL R E L DATE R E L DATE P A N E L HO D A YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER 1 E 65ICD7001 1 R ------ L C 3 9 DA.TA TRANS S Y S ( W 1 D E BAND) NO TRN-CCBD ENTERED 02-02-65 LOFC 230-390 KSC-F 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 KSC 03-23-65 LOFC 230-390 03-15-65 LOFC 230-390 KSC-EDV- 08-13-65 LOFC 100-390 KSC-EDV- 02-08-66 LOEL 230-390 KSC-LVO- 04-28-65 LOFC 230-390 KSC-F NO IRN-CCBD - - --.------ -dm---- R PREPARIi I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T E V I T ' ------. --&----------we ENTERED A 65ItD7002 - L C 3 9 OPNL I N T E R C O M SYS-S/C 65ICD7003 - L C 3 9 FAC I N S T CABLING-LOC/ROUTING ESE/GSE E 65ICD7006 A L C 3 9 S A T V TRANSP ROUTES -S/C D 65ICD7010 A L C 3 9 SAT V VEH STAGE + S/C S/C MISALIGNMENT . KSC-F A L C 3 9 CSM + LEM T O F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD EbJTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED , NO IRN-CCBD ENTERED - S/C . GSE TO HAZARD PROOF MON S Y S T v L C - 3 9 A L C 3 9 V A B H I G H BAY AREA TO S / C ' .- �DATE 2 9 J U L 66 AS -- --- -- D S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E -- - .................... R DOC REV 502 ----- DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD - SCHED ACTUAL R E t D A T E R E L DATE P A N E L MO DA YR KO D A YR CODE --- ....................................... 4 PAGE 1 CONT, - - 501-66-0397 C-S 000-100 MSFC C-S 000-100 MSFC-AST 03-18-65 EI 300-230 MSC L V E S E I P R O P Z t L A N T SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 12-15-65 E I 220-210 MSFC-AST L V E S E TO LAUNCH EQUIPMENT ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 12-09-65 E I 220-210 MSFC-AST EI 230-220 EDS L I M I T S E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 - 08-06-65 04-01-67 COMP I N T F A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - - -------- -------- ------ -------------- ------- B D E S I G N C R I T E R I A FOR SATURN V ONBOARD EDS ICD-CCBD 5 0 1 - 6 6 - 0 0 7 8 A 13M65502 PREPARIN I N T E R F A C E AREAS CE?2TER OR CEI NUMBERS A C JITY COMP I N T E R F A C E 04-15-66 SC E S E TO L V E S E - MSFC-AST - I N S T U N I T T O SPACECRAFT E L E C REQ ICD-CCBD 5 0 1 - 6 6 - 0 1 4 8 04-05-65 EX 000-100 MSFr-AST - DES OF S A - 5 0 2 AND S C - 0 2 0 ICD-CCBD 501-66-0160 IRN-CCBD 5 0 1 - 6 6 - 0 1 6 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 5 1 01-14-66 CS 000-100 HSFC-AST - EDS 10-31-66 EDS CHECKOUT SCHEMATICS LC39 S I T E P L A N + GENL ARRANGE-S/C GSE 01-28-65 EI 000-220 MSFC LOFC 230-390 KSC-F : �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl PAGE DATE 2 9 J U L 66 -- --- -- C H C DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV , - DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L DATE R E 1 DATE P A N E L MO D A YR M O CIA YR CODE -------- -------- -I---- PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T X V I T -------------- ------ L A U VEH/SPACECRAFT PROCEDURAL R E 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 0 0 L A U VEH TO SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 6 NO IRN-CCBD ENTERED 8 ENVELOPE L E M / S - I V B I I U CLEARANCE P H Y S I C A L ICD-CCBD 5 0 1 - 6 6 - 0 0 9 9 - I U TO SPACECRAFT PHYS REQ IRN-CCBD 5 0 1 - 6 6 - 0 1 0 3 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 1 SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 1 PHY REQ B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 - EMI COMPATIBILITY DESIGN ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 CRITERIA L V TO S C 0 2 0 I N S T R + COMM I N T E R F A C E ICD-CCBD 5 0 1 - 6 6 - 0 0 7 3 NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 0 7 3 , IRN-CCBD 501-66-0073 000-100 MSFC 000-100 MSFC-AS 000-100 HSFC-AS �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS DATE 2 9 JUL 6 6 -- --- -- D S DOCUHENT NUMBER* OR R E V I S I O N N O T I C E DOC REV 501 ----- _ -------------------- --- ........................................ R 1 J 65ICD9773 DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD - 651CD9776-001 --- SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR M O D A YR CODE -------- ---a_- ----I--- PREPARING I N T E R F A C E AREAS CENTE" OR C E I NUMBERS A C T I ' - Y --------------- ---------- 501-66-0129 P I P C R I T S - I C F L U S H + PURGE U N I T SAT V ICD-CCBO 5 0 1-66-0047 02-07-66 LO-FA 010-390 MSFC-EDV PHY I C D + P I P E C R I T S I I L E A K DETECT SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 4 IRN-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-10-65 LO-FA 020-220 MSFC-EDV 02-10-66 LO-FA 010-220 MSFC-E DV PHY I C D P I P E C R I T S I C FWD ICD-cECBD 5 0 1 - 6 6 - 0 1 8 0 U M B SERV UN SV SEE-DWG SEE B A S I C NUMBER FUR R E V I S I O N p T I T L E o ETCa - PHY I C D + P I P C R I T HAZ GAS ANALYZER SATV ICD-CCBD 5 0 1 - 6 6 - 0 1 0 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 5 02-04-66 LO-FA 220-000 MSFC-EDV A L C 3 9 M t PHY LOC PORT I U WATER ACCUM CART ICD-CCBD 5 0 2 - 6 6 - 0 2 0 7 03-02-66 LO-FA 220-390 KSC-EDV 02-08-66 LOFC 230-390 KSC LOFC 230-390 KSC-EDV-2 66ICD7007 - LC-39 66ICD7009 - L C 3 9 S/C A 80H90501 P A G E 121 CONT, HAZARD PROOFING-S/C DeC. POWER S U P P L I E S A F L I G H T MECHANICS P A N E L I C D 01-20-66 �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE DATE 2 9 J U L 66 -- --- -- ; 7 P - D O C U M E N T NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD . -. J 65iCD9765 I - R R 1 2 6 5 ICD9766-001 * - - ICD-CCBD IRN-CC8D IRN-CCBD -------- -------- PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT --------------- ------- ---I 501-66-0130 501-66-0300 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T . * SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO D A YR CODE V 06-2 5 - 6 5 LO-FA 220-390 KSC-P+VI 02-11-66 LO-FA 220-390 MSFC-E D\r 50 1 - 4 5 - 3 1 501-66-0295 501-66-0131 PIPING CRITERIA S - I 1 ICD-CCBD 5 3 1 - 6 6 - 0 0 4 5 IRN-CCBD 50 l - 6 6 - 0 3 2 7 PNEU SYS/SATURN V SEE-DWG SEE B A S I C NUMBER FOR R E V I S I O N o T I T L E e E T C m PHYS I C D . S - I C H Y C R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 02-10-66 LO-FA 220-390. KSC-K-Dl PHY I C D S - I C PNEU CONSOLE RKS 1-2-3+4 ICD-CCBD 5 0 1 - 6 5 - 6 1 09-15-65 LO-FA 220-390 KSC-K-Dl PHY I C D PNEU CONSOLES 5 9 6 ~ 7+ 8 S - I C ICD-CCBD 5 0 1 - 6 5 - 3 4 08-09-65 LO-FA 220-390 KSC-P+Vf PHY I C D S - I C PNEU CHECKOUT RKS 1-2-3+4 ICD-CCB'D 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 MSFC-ED\ PIPING CRITERIA S-IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 220-280 MSFC-P+\ 12-09-65 LO-FA 210-390 KSC-EDV PNEU CONSOLE SET A S-11 STAGE GSE PLACEMENT ON MBL LAUNCHER' ICD-CCBD 501-66-0129' - . �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 1 1 DATE 2 9 J U L 6 6 -- -- --- -- .- D S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E - .................... DOC REV --- --------------------------------------- J 651CD9757 R DOCUMENT T I T L E OR CCBD NUMBER - 2 - - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO D A Y R MO DA YR CODE -------- 09----- ---s-- PREPARING I N T E R F A C E AREAS CENTER ACT ' I T Y OR C E I N U M B E R S - ----------s- --I ----- 06-21-65 LO-FA 220-390 KSC-P+VE PHY I C D I U C O O L I N G U N I T + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 09-15-65 LD-FA 220-390 MSFC-EDV PHY I C D I U PNEU CONS ICD-CCBD 5 0 1 - 6 5 - 4 8 IRM-CCBD 5 0 1 - 6 6 - 0 2 9 2 09-1 5-65 LO-FA 220-390 PISFC-EDV 06-21-65 LO-FA 220-390 KSC-P+VE P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 02-10-66 LOFA 220-390 MSFC-EDV PHY I C D S - I C I N E R T P R E F I L L + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 7 09-15-65 LO-FA 220-390 MSFC-EDY PHY I C D S - I 1 PNEU CONSOLES S 7 - 4 1 B / S A T ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 501-66-0124 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE PHY I C D S - I V B H T EXCH D S V - 4 8 - 4 3 8 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 6 9 V PIPING CRITERIA P H v I C D APS PNEU CONS DSV-4B-436/SAT ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 PHY I C D S I I PNEU CONSOLE S 7 - 4 1 C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 50 1-66-0294 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 1 D / S A T ICD-CCBD 50 1 - 6 5 - 3 0 V V V V 06-25-65 LO-FA 220-390 KSC-P+VE �. APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl DATE 2 9 J U L 66 PAGE -- --- -SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE C H G DOCUMENT NUWBERo OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD IRN-CCBD - - J 651CD9755 i) R 3 - -------- -------- ------ --------------- ------- 501-66-0126 501-66-0126 U M B I L I C A L + S E R V I C E CONN S - 1 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED UMB + SERV CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 8 FORWARD AFT U d B + S E R V l C E CONNECTIONS S - I V B ICD-CCBD I RN-CCBD PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVIT FORWARD 06-2 8-65 LO-F A 020-390 KSC-P+VI 06-21-65 LO-F A 040-390 KSC-P+VI 06-1 8 - 6 5 LO-FA 040-390 KSC-P+V 06-18-65 LO-FA 090-390 KSC-P+V 501-66-0177 501-66-0283 U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 5 IRM-CCBD 5 0 1 - 6 6 - 0 2 8 4 PHY I C D S - I V B PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 V 06-21-65 LO-FA 220-390 KSC-K-D PHY I C D S - I V 8 PNEU CONS D S V - 4 8 - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V 06-21-65 LO-FA 220-390 XSC-P+V 0 1 - 2 8-66 LO-FA 020-390 P I P I N G CRITERIA S-IVB I CD-CCBD 50 1 - 6 6 - 0 0 4 3 , IRN-CCBO 5 0 1 - 6 6 - 0 3 7 4 PNEU CONS SET L C 3 9 - KSC-P+V �IA 0 1 APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 J U L 6 6 AS -- --- -- O S DOC!%IMENT NUMBER, OR R E V I S I O N NOTICE DOC REV - 501 ----- -- SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO DA Y R CODE DOCUMENT T I T L E OR CCBD NUMBER - - ------------------- --- ....................................... - UMB + SERV CONNS P L A T E NO 3-2 S - I C PAGE 1 1 CON?, PREPAR I N ( INTERFACE AREAS CENTER OR C E I NUMBERS ACT ' I T Y - -------- -------- ------ -------------- --AFT 08-10-65 LO-FA 08-10-65 LO-FA ---_.)__ 010-210 MSFC-P+VE 010-390 KSC-P+VE ICD-CCBO 5 0 1 - 6 5 - 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD-501-66-0382 - - - MOTION ENV AFT UMB PLATES 1 , 2 9 4 3 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 S-IC PHY I C D LAU VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 6 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 0 IRM-CCBD 5 0 1 - 6 6 - 0 2 9 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 I N T K UMB/LC39 GSE 08-09-65 LO-FA PHY I C D LAU VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 7 IRN-CCBO 5 0 1 - 6 6 - 0 1 9 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO IRN-CCBD ENTERED FWD U M W L C 3 9 GSE 08-09-65 LO-FA 06-28-65 LO-FA U M B I L I C A L 9 SERV CONN S I I L O X DISCONNECT ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-21-65 LO-FA U M B I L I C A L 4 SERV CONN S - I 1 06-21-65 LO-FA UMB + SERV CONNECTIONS S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 3 INTERM LH2 DISC . �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 2 9 JUL 66 AS -- --- -- D 5 DOCUMENT NUMBER* O R R E V I S I O N NOTICE A 65ICD9404 R 1 R R DOC REV - 2 4 - - - 501 ----- DOCUHENT T I T L E OR CCBD NUMBER CONTo : PAGE SCHEO ACTUAL REL DATE REL DATE PANEL MO DA YR HO DA YR CODE -------- ------- ------ PREPARIE INTERFACE AREAS CENTER OR C E I NUMBERS A C T I V I T I - ------- --I---------- FUNCT I N T F F L U I D REQHTS L H 2 SYS SAT V IRN-CCBD 5 0 1 - 6 6 - 0 0 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-2 8 - 6 5 LOPG 010-250 KSC-P+Vt FUNCT I N T F F L U I D REQHTS LOX SYS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 06-03-65 LOPG 010-250 KSC-P+Vf 06-1 5 - 6 5 LOPG 010-250 KSC-P+Vi FUNCT I N T F F L U I D REQMTS V A B ECS 'SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED 05-X 9 - 6 5 COPG 000-260 KSC-K-Dl P I P C R I T APS PROP S E R V I C I N G SAT V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-ED! UMB AND SERV CONN P L A T E 3-4 ICD-CCBD 5 0 1 - 6 5 - 4 0 1RN-CCBD 5 0 1 - 6 6 - 0 2 9 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 0 8 - 1 0-65 LO-FA 010-210 KSC-P+VE 03-18-65 LO-FA 010-210 KSE-P+VE SYS SAT V FUNCT I N T F F L U I D REQHTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 1 * S I C AFT UMB SERV CONNS P L A T E NO 1-2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRM-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 50 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 ' S-IC AFT �APOLLO INTERFA'CE CONTROL DOCUMENT LOG DATE 2 9 J U L 66 .. AS -- --- -- D S DOCUMENT NUMBERV OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD - "' - 50.1. ----- PACE I CONT, - SCHED ACTUAL R E L D A T E RE^ DATE PANEL M O DA YR MO DA YR CODE PREPARIN, I N T E R F A C E AREAS CENTER OR C E I NUMBERS AC 'ITY -------- ------- ------ --------------- ---em--- 501-66-0122 501-66-0265 MSFC COUNT CLOCK TO KSC T I M I N G L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 0 9 8 08-14-65 LOEL 200-390 MSFC-AST L V E S E TO K S C DATA MEASUREMENTS 0 2 - 1 1-66 LOEL 220-290 MSFC-AST LOW BAY ESE TO I N S T R U SYS + REC ICD-CCBD 501-66-0171 02-11-66 LO-EL 220-290 MSFC LOW B A Y E S E TO I N S T R SYS AND REC ICD-CCBD ' 5 0 1 - 6 6 - 0 0 8 2 02-1 1-66 LO-EL 220-290 MSFC-AST S E R V I C I N G REQMTS ECS S A T V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 I RN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-03-65 LOPG 250-390 MSFC-KSC FUNCT I N T F F L U I D REQMTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 - LOPG 4 �, I A0 L APOLLO I N T E R F A C E CONTROL DOCUHENT LOG DATE 2 9 J U L 66 I I- DOCUMENT NUMBER, OR R E V I S I O N N O T I C E _- _ .................... S E 65ICD9020 E 65ICD9041 : PAGE -- --- -- , DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - L C 3 9 VAB H I G H BAYS TO L / V ESE/GSE - - - -------- --.=.----- 1-0--- PREPAR I F I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I T Y - -e------------- ------- 11-19-65 LOFC 220-390 KSC-F LC 3 9 VAB L O W B A Y A R E A T O L/V-ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-EDV- L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-EDV- L C - 3 9 PAD AREA L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EDV- S - I C / M L HOLD DOHN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC 220-390 MSFC LOFC 000-040 MS FC 03-09-66 LO-EL 220-390 MSFC-AS7 L V ESE TO RANGE SEQUENCING L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 6 - 0 0 6 2 08-14-65 LOEL 220-390 MSFC-AST L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 02-11-66 LO-EL 220-370 MSFC-AST L V ESE YO I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 02-11-66 LO-EL 220-290 MS FC-AST - . WIND LOAD A L L E V I A T I O N S Y S F A C I L ' T ' O L P V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E E S E ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE 09-0 1-66 �APOLLO I N T E R F A C E DATE 2 9 J U L 6 6 CONTROL DOCUMENT LOG AS 501 CONTO SCHED D S DOCUEENTNUMBERo OR R E V I S I O N N O T I C E R DOC REV DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD 4 - E 6 5 ICD8002 A S/C LC/34/37/39 AoC. - TIMING POWER REC- LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 4 COUNTDOWN D I S T + CONN GSE SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED 09-22-64 LO-FC 230-340 11-29-65 LOFC 230-347 05-03-65 LOPG KSC-K-DT 10-01-64 LOFA MSC-FO-HJE KSC-EDV-2 KSC-EOV LEM SWG ARM UMB D I S C A 1 4 - 1 7 2 LC34/37/39 KSC-0 CMD MOD ACCESS ARM C A B L I N G MSC-FO VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP - - ENTERED FUNCT I N T F REQMTS ECS MC .LEM S / C 8 LC37/39 - PREPARING I N T E R F A C E AREAS C E N T F R ACT1 i Y OR CEZ NUMBERS PEM U M B I L I C A L AND T E S T CABLES FOR L C 3 9 NO IRN-CCBD ENTERED A 65ICD8001 - ACTUAL R E L DATE R E L D A T E PANEL HO DA YR MO DA Y R CODE 2 3 AFRM 9 T O ACCESS ARM WHT RM C / M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 HSC-EDV PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER 12-1 0 - 6 5 LO-FA 110-300 KSG-EDV 02-02-66 LOFC 220-390 YSFC SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 �APOLL(1 I N T E R F A C E CONTROL DOCUMENT L U G D A T f 2 4 JUL 6 6 -- -....- -.- PAGE C DOCUMENT NUMBER, OR R E V I S I O N N O T I C E I I _-__ -- -..--.r -----.=----.. A 651CD7666 *----- DOC REV DOCUMENT T I T L E OR CCBD NUMBER --..-. ....--.---., - -...- .---.---.._-. I - T.CIC I -.-. ._.--.=..-- FUNCY I N l F REQS ECS L C 3 5 PAD 8 S/C.-GSE B L C 3 9 i L T GSE SYSTEMS AFRR C O N F I G NO IRN-CCBD ENTEREO NO TRN-CCBD ENTERED NO I R h - C C B D ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CC&D E N i E R E D NO IRN-CCBD ENTERED - J. 65ICD7788 - J 65ICD7790 1A R R R 2 3 - L C 3 9 A M L P I P C R I T 4- l N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED SCHED ACTUAL R E L DATE RE: DATE PANEL MO DA YR MO D A Y R CODE -.-- ,. . -.. . * . ..- -.- - . -.. . . , I 03-19-65 PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVlf -.. LOPG 1 1-0 5-64 LO-FC ,---..'I ---,----- ------- 100-390 KSC-K-0 230-390 MSC-HAA .. F L SYS 08-20-65 LOFA 230-3'30 KSC-EDV 11-17-64 LOFA 230-390 KSC-DE L C 3 9 PHY I N f F C GOX COND PNL L E A K TS U N I T NO IRN-CCBD ENTERED 07-22-65 LOFA 230-390 KSC-EDV ACCESS ARM + SERV MODULE CABLE REQMTS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED ' 09-22-45 LOFA 230-390 KSC-EDV LC39-LUT GSE CABLES-GAS N I T SYS - �A P O L L O INTERFACE AS DATE 2 9 J U L 66 -- --- -- D _ DOCUMENT NUMBERS 2% R c V I S I O N NOTICE _ _-____ S _.= _ 9 _ C _ _ _ _ _ C - - CONTROL DOC REV ---.- 501 DOCUMENT T I T L E OR C C B D NUMBER -~*~--------O~I.=---G~---Y.=F-L~=~IY-.-----.i.---~-. DOCUMENT :a~ LOG 1 CON?" ---- SCHED ACTUAL REL. D A T E R E C D A T E P A N E L MO DA VR P O D A 'iR C 3 D E em- ------=. -.=- -.--.. :.iC.C: Pa.-PIY PREPAR I X G I N T E R F A C E A R E A S CENTE!? OR C E I hlUMBE9S _ CY~P--iU--L-L-C.-.-~- # . -.- -.= 2.-- NO IPN-CCDD NO XRN-CCBD ENTERED ENTERED NO J R R - C C B D ENTERED h i 0 1 RN-CCSD ENTERED NO ! R N - C t B O ENTERED NO 1 R ~ - C C B D ENTERED NO IRN-CCBD E N T E R E D NO IRN-CCBD E N f ERED - F 65fCD7468 - C 65ICD7567 C 65ICD7568 LC34 P I P I N G NO IRN-CCBD NO IRN-LCBD NO IRN-CCBD -NO IRN-CCBD NO IRN-CCBD CRPT + I N T F LOC SCC F L D S Y S ENTERED ENTERED ENTEREO ENTERED ENTERED + ZNTF L O C 140-390 KSC-EGi, LOFC. 230-390 KSC-F 03-13-65 LOPG 100-390 KSf 12-02-65 LOPG 01-12-65 FUNCT I N T F REQS E C S L C 3 9 P A D A SIC-GSE NO I R N - C C B D ENTERED LC39tMSS P I F C R i T L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD E M F L D SYS , ENTERED ENTERED ENTERED '-DT - FUNCT I N T F R E Q M T S GHE LC39A S I C G S E 05-02-86 LOPG 100-390 K S C - EDV FUNCT I N T F REQMTS G N 2 L C 3 9 A S L C GSE 05-02-66 LCPG 100-390 KSX-.K-DT LC39A S / C G S E FUNC I N T F R E Q c G O X 02-09-66 LOPG 230-390 KSC-EDV - LC39 LOFC 230-330 KSC-F - PAD B 0 6 - 0 1-66 �APOLL.0 I N T E R F A C E CONTROL DOCUMENT. L O G PAGE 1 D A T E 2 9 J U L 66 .-- ..-.- C S _ & _ DOCUMENT NUMBER? D K R E V I S I O N NOTICE -* -_.... R R R R R *---- .O-EU.CO---.C-L-- - -DOC REV -. -.. 12 14 16 A 65ICi17052 DOCUMENT T I T L E OR CCBD NUMBER --<.. . -_-.^ NO NO NO NO NO 9 k l - SCHEO ACTUAL R E L DATE REQ DATE PANEL MO DA YR MO DA YR CODE - .:.-...-. E RN--CCBD IRN-CCBD IRN-CCBD IRN-CCBD fRN-CCBD -2-.- -~.-.-.l.~-.._~.-.-,T,-C..T.L-..m-C,-7.-- .... .i.-.C.--C A 65ICD7167 -r-<-.....--. . . . . - . ~ ~ --99---- 02-08-66 LOEL 230-330 KSC-LVO- 04-28-65 LOFC 230-390 KSC-F FUNCT I N T F REQS ECS L C 3 9 VAB S I C - G S E 03-19-65 LOPG 100-390 KSC-K-01 FUNCT I N T F RQMTS ECS L C 3 9 / V A B LEM SC GSE 05-03-65 LOPG 230-390 KSC-K-Dl L C 3 9 LCC F A C I L I T Y S / C E S E I G S E NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 03-05-65 230-390 KSC-F SC ! GSE TO HAZARD PROOF MON SYSTBI<-39 L C 3 9 VAB H I G H B A Y A R E A TO S / C NO TRN-CCRD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - -_r-----.- - ENTERED ENTERED ENTERED ENTERED ENTERED A A 65ICD7166 ----._i--_. PREPARIA I N T E R F A C E AREAS CENTER OR C E T NUMBERS ACTIVITY A LC39 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED .. 01-25-65 LOFC 230-390 KSC-F �PAGE DATE 2 9 JUL 56 -- O S -- - -==- -- DOCUMENT NUMBERf 24 R c V I S l O N NOTICE -C-------OUe--F._I-U.--s DOC REV PC- DOCUMENT T I T L E OR C C 5 D NUMBER --- ---e --------~OL-CCC-PC.-O.-~-.~C-.-.~L---LC-C<-------=-. ICD-CCBD - ACT'Jnk. SCHED R E L D A T E RE& D A T E P A N E L M O D A "R Y O 0 4 YR CODE .s---. -. .- -.--. ---= LC -- ? R E P A ! ? IFv\ ENTERFACE PqEaS C E h T E R OR C E X N U M B E R T A C Y L V I T ~ -. . - - .-e-------.- c 501-66-0060 EDS CHECKOUT S C H E M A T I C S ZCD--CCBD 501-56-GO61 f~~-~68~'50h-66-006~ I2N-CCBD - 501-46-0276 L C 3 9 S I T E P L A N a G E N L ARRANGE-S/C NO I R N - C C B D E N T E R E D GSE 01-28-65 LOFC 230-.3'30 KSC--F L C 3 9 DATA TRANS S Y S I W I D E BAND] NO I R N - C C 8 D E N T E R E D 02-02--65 iOfC 230-390 KSC-F L C 3 3 OPNL INTERCOM SYS-S6C 02-06-65 LOFC 230-396 KSC-F 02-08-66 LOFC 230-340 KSC 03-23-65 LOFC 230-330 KSC-F 03-15-65 tOF6 230-390 KSC-EE'J- 08-13-65 LOPC 100-390 XSC-EDV-. 08-24-65 LOEL 230-390 KSC-VG-2 ESE6-GSE L C 3 9 FAC I N S ? CABLING-tOG/ROUTING L C 3 9 OPNL B V SYS-FAC-SIC SIC ESEiGSE A L C 3 9 S A T V T R A N S P ROUTES -SPC A L C 3 9 S A P V VEH S T A G E 4 SPC MISALIGNMENT A L C 3 9 C S H a LEN TO F A C I L I T Y CABLES NO I R N - C C P D E N T E R E D NO IRN-CCBD E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D NO I R N - C C B D E N T E R E D I �A P O L I - 0 I N T E R F A C E CONTROL DOCUMENT L O G D A T E 2 9 JUL 66 - ...... .- AS ..... 501 ....-....... - IAOl CONY, PAGE 4 C H 7 ___ _S DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E -_.__-__-.-.. DOC REV ..-..--.-..__----...- DOCUMENT T I T L E OR C C B D NUMBER I . . --w."rC . . . > .. -"-.OY.*.. ..-..-. .........................I...............,... -.., . ACTiJAL PREPAR SCHED I N T E R F A C E AREAS CENTER R E L D A T E R E L DATE P A N E L OR C E I NUMBERS A C T f V I : MO DA YR HO D A YR CODE .__ __.*-----".*. . .......... . -..,.~-...--.--1.-.-C.- .-.I- ------- ( . I R 2 3 R 4 R - ~ t A 13M65001 IRN-CCBD IRN-CC.BD IRN-CCBD B D E S , I G N C R I T E R I A FOR S A T U R N V 3 N B O A R D EDS ICD-CCBD 501-66-0078 A 13M65501 - A 16331-63A107350 - A 16331-63A107393 501--66--0074 501-.66-.0074 501-46-0392 - - MSFC-A! 300-230 MSC 300-100 MSC 220-230 MSFC-A! LV E S E / P R O P E L L A N T S Y S T E M S ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 220-210 MSFC-A! L V E S E TO L A U N C H E Q U I P M E N T ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 220-210 MSFC-A! E t E C XCD ACE SPC-LPV ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 S A T V LV ICD-CCBD 1 RN-CCBD IRN-CCBD COMP X N T F COMP I N T E R F A C E ESE TO APOLLO S t C ESE 501-65-85 501-66-0192 501-66-0192 A DEF S A - 5 0 1 4 SC-017 ICD-CCBD 5 0 1 - 6 6 - 0 1 4 6 - C-S 000-100 EDS L I M I T S A SOFTWARE I C D - A C E S / C - L f V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 - 08- 06-65 ELECTRICAL INTERFACE 4 D E S OF S A - 5 0 1 AND S C - 0 1 7 EDS .. 000-100 MS FC-A! �. A P O L L O I N T E R F A C E CONTROL OOCUNENT L U G SCHEO ._ U S - DOCLHENTNUMBER* OR R E V I S I O N NOTICE -I------------------ REV --- - DOCUMENT T I T L E OR CCBD NUMBER ----------------------------------,------- L A U VEHISPACECRAFT PROCEDURAL REQ IRN-CCBD 501-66-0200 L A U VEH T O SPACECRAFT FUNCTIONAL REQ ICD-CCBD 501-66-0336 NO IRN-CCBD ENTERED A I U 10 SPACECRAFT PHYS REQMTS ICD-CCBD 501-66-0103 IRN-CCBD 501-66-0103 IRN-CCBD 501-66-0103 IRN-CCBD 501-66-0103 IRN-.CCBD 501-66-0386 - SPACECRAFT TO Q-BALL PHYS REQ ICD-CCBD 501-66-0112 IRN-CCBD 501-66-0112 IRN-CCBD 501-66-0112 XRN-CC8D 501-66-0112 0 ENVELOPE L E H / S - I V B I I U CLEARANCE P H Y S I C A L ICD-CCBD 501-66-0099 8 SATURN/APOLLO FREQ PLAN ICO-CCBD 501-66-0256 - - ACTUAL R E L DATE R E L DATE PANEL DOC EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 201-66-0114 L V T O SC 017 I N S T R + COHH INTERFACE ICD-CCHD 501-66-0074 I R N - C C D O 501-66-0074 MO DA YR MO OA YR CODE --------------- ------ PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACT7 ' T Y -.D.---P-..-.-N..D---- P-VC I--- �APOLLO I N T E R F A C E CONTROL DOCUHEN T LOG IAOl DATE 2 9 J U L 66 PAGE -- --- -- C H CI DOCUMENT NUMBER* OR R E V I S I O N N O T I C E _-- - .................... 3 R DOC REV --- 1 J 65IC08303 R 1 R 2 DOCUMENT T I T L E OR CCBD NUMBER ----------------_---o--------------- NO IRN-CCBD , - - SCHED ACTUAL R E L DATE R E L D A T E P A N E L HO DA YR I40 D A YR CODE --we--- C / H ACCESS ARM ADPT HOOD TO S / C S-IB -me---. --C--------C)-- ------. ENTERED VERT STOP FOR L E S ACCESS ARH NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED LC34/37 ..----.--- PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I ' L/V+S/C HISALIGN, I N T F RE0 FOR SAT I B VEH L V PROTUBERANCES L C 3 4 / 3 7 PHY I N T F R E T R A C T I O N MECH 0-BALL fCD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER PHY I C D CALOPS CHECKOUT CONSOLEPSAT-IB PHY I C D HAZARDOUS GAS ANALYZER SATURN I B ICD-CCBD 2 0 1 - 6 6 - 0 1 0 2 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 7 9 LOW BAY ESE T O I N S T R U SYS ICO-CC.00 5 0 1 - 6 6 - 0 1 7 1 + REC 11-1 8 - 6 4 LOFA 230-300 HSC-FO 11-04-65 LOFA 100-300 MSC-EDV O ? - O ~ - O ! ~ LO-FC 200-367 ns~c-P+ LOVC 12-10-65 LO-FA 110-300 KSC-EDV LOFA 220-347 HSFC-EL: 12-10-65 LO-FA 220-347 MSFC-EE 02-11-66 LO-EL 220-290 HS FC 12-01-65 501-66-0039 MSFC 07-01-65 �9 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 6 6 O S -- DOCUMENT NUMBERo OR R E V I S I O N N O T I C E --s---------------e- P A G E LO -- DOC REV DOCUMENT T l T L E OR CCBD NUMBER --- ...................................... NO IRN-CCBD NO IRN-CCBD SCHED ACTUAL R E L DATE R E L ' D A T E PANEL HQ DA Y R MO DA YR CODE P P P - Y - - - -----I-- .Do---- PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACT ? T Y - -PO-----Y--C2QP c--------- ENTERED ENTERED F 651CD6068 A P I P C R I T + I N T F LOC S I C F L D SYS L C 3 7 8 SS 09-14-65 LOPG 100-230 KSC-EDV F 651CD6069 A L C 3 7 8 S A T I B SS P I P C R I T LEM F L D SYS 05-16-66 tOPG 230-37C KSC-EEV C 65ICD6467 - FUNCT I N T F REQMTS GHE L C 3 7 B S / C GSE 05-02-66 LOPG 100-370 KSC-EDV FUNCT I N T F REQMTS GN2 L C 3 7 B S / C 05-02-66 LOPG 100-370 KSC-EDV 11-1 0 - 6 5 LOFA 230-370 KSC-EDV L C 3 7 SS TO L / V ESE/GSE ICD-CCBD 201-66-0113 12-08-65 LO-FC 220-370 KSC-EDV-2 L C 3 7 PAD AREA E S E / G S E - L f V ICD-CCBD 201-66-0204 IRN-CCBD 2 0 1 - 6 6 - 0 2 0 4 02-10-66 LO-FC 220-370 KSC L C 3 7 PHY I N T F S - I B STAGE TO HOLDDOWN ARM ICD-CCBD 2 0 1 - 6 6 - 0 1 0 1 01-1 0-66 LO-FC 000-370 KSC-EDV 09-22-64 LO-FC 230-340 10-01-64 LOFA 230-340 MSC-FO-HJ 03-07-66 LOFA 230-340 KSC-EDY 11-17 - 6 4 LCFA 100-300 MSC-NBA- C 65ICD6468 - 378 PHY l N T F LEM UMB ARM C A B L E REQMTS NO IRN-CCBD F 651CD6671 A 65ICD8001 - LC/34/37/39 - ENTERED - T I M I N G + COUNTDOWN D I S T L C 3 4 / 3 7 8 3 9 SM SWG ARM U H B D I S C A 1 4 0 1 9 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED B LC37/39 J 65ICD8302 GSE LEM SWG ARM UHB D I S C A14-172 LC34/37/39 CMD MOD ACCESS ARM C A B L I N G ' - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS DATE 2 9 J U L 66 -- "..-- -- 212 --...-- W P DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E _-- - .................... * 9 9 9 * 4 J 651CD5892 R 1 R 2 R 3A R R DOC REV --- PAGE CONTO C G IAOl DOCUMENT T I T L E OR CCBD NUMBER ----------------------=----------------- SCHED ACTUAL R E L D A T E R E L DATE PANEL WO DA YR MO DA YR CODE -------- PREPARI I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTXVXT ------- ----------a---- 0----0-- ---0-0 08-02-65 LO-FA 010-347 KSC-P+V PHY I C D BOAT T A I L COND UM8LS S - 1 8 / 1 8 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 0 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 0 08-02-65 LO-FA 010-347 KSC-P+V A A PHYS I C D I N S T R U N I T PNEU C O N S O L E / I S ICD-CCBD 2 0 1 - 6 6 - 0 2 8 2 NO IRN-CCBD ENTERED .. IRN-CCBD 2 0 1 - 6 6 - 0 2 8 2 03-02-66 LO-F A 220-347 KSC-P+V P I P I N G C R I T E R I A INSTRUMENT U N I T L C 3 4 - 3 7 ICD-CCBD 2 0 1 - 6 6 - 0 1 4 4 IRN-CCBD 201-66-0238 12-30-65 LO-FA 220-347 MSFC-K-' A PHY I C D I U C O O L I N G U N I T L C 3 4 ALTERNATE NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 3 03-02-66 LOFA 220-347 HSFC-K- A PHY I N T F CONT DWG I U FLOW CONT V A L V E BOX ICD-CCBD 2 0 1 - 6 6 - 0 1 0 4 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 9 12-16-65 LO-FA 290-347 02-08-66 LOFC 230-370 - 4 5 - PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED ENTERED ENTERED FWD CSW ARM = 1 1 A PHY I C D S - I V B I I U C O O L I N G U N I T / I B NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 3 7 - - KSC-P+VI . LC 37 HAZARD PROOFING S / C . KSC �t APOLLO 1NTERFAC.E CONTROL DOCUMENT LOG DATE 29 J U L 66 P A G E LO' --. -- --- -- D S DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER IRN-CCBD IRN-CCBD SCHEO ACTUAL R E L D A T E R E t . D A T E PANEL MO DA YR HO 08 YR CODE PREPAR I X G INTERFACE AREAS CENTER OR C E I NUMBERS ACT- ITY 201-66-0235 201-66-0281 A PHY I C D A F T UMB S W I N G ARM NO 2 S - I V B NO IRN-CCBD ENTERED 01-21-66 LOFA 040-347 HSFC-K-CT A PHY I C D FWD UMB SWING ARM NO 3 S - I V B ICD-CCBD 2 0 1 - 6 6 - 0 2 9 0 NO IRN-CCBD ENTERED IRN-CCBD 2 0 1 - 6 6 - 0 2 9 0 01-21-66 LO-FA 040-347 MSFC-GT A PHY I C D I U UMB SWING ARM NO 3 IRN-CCBD 2 0 1 - 6 6 - 0 2 8 6 03-1 5-66 LOFA 090-347 MSFC-K-DT 08-02-65 LO-FA 0 10-347 KSC-P+VE 08-02-65 LO-FA 010-347 KSC-P+VE - PHY XCD UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S I B / I B ENTERED ENTERED ENTERED PHY I C D UMB NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD CONN S - I B / I B ENTERED ENTERED ENTERED ENTERED ( S H C MAST111 SH M A S T I V PHY I C D 0 8 A T T A I L L O X U H B S - 1 8 / 1 6 ICD-CCBD 2 0 1 - 6 6 - 0 2 8 4 IRN-CCBD 2 0 1-66;0284 P H Y S I C A L I C D BOAT T A I L FUEL UMB S - I B / I B ICD-CCBD 2 0 1 - 6 6 - 0 2 7 8 IRN-CCBD 2 0 1 - 6 6 - 0 2 7 8 ' 08-02-65 LO-FA 010-347 KSC-P+VE �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 C cI G AS 212 PAGE CONTO SCHED DOCUMENT NUMBER, DOC OR R E V I S I O N N O T I C E REV I - - I N T E R F A C E AREAS CENTER OR CEX NUAaERS ACTIVII ------------------- -------- ------- -.----- L V ESE T O R A N G E SEQUENCING L C - 3 4 ICD-CCBD 2 0 1 - 6 5 - 0 0 3 6 05-28-55 LO-EL 220-340 HSFC-AS L V ESE T O F A C I L I T Y AC POWER L C - 3 4 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD E N T E R E D 08-12-65 LOEL 220-340 ('4sFC-AS 02-1 8-66 LO-EL 220-200 MSFC-AS MSFC COUNT CLOCK T O KSC T I M I N G ICD-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 IRN-CCBD 2 0 1 - 6 5 - 0 0 3 9 06-08-65 LO-EL 200-240 >tSFC-AS L V ESE TO KSC DATA MEASUREMENTS ICD-CCBD 2 0 1 - 6 6 - 0 1 4 6 IRN-CCBD 2 0 1 - 6 6 - 0 1 4 6 12-15-65 LO-EL 220-340 MSFC-AS L V ESE 10 WATER DELUGE SYSTEM ICD-CCBD 2 0 1 - 6 5 - 0 0 4 0 I RN-CCBD 2 0 1 - 6 5 - 0 0 4 0 05-28-65 LO-EL 220-340 HSFC-AZ 11-10-65 LO-FA 040-347 HSFC-EE DOCUHENT T I T L E OR CCBD NUMBER A L V E s E TO I N S T R SYS + RECORDERS ICD-CCBD 2 0 1 - 6 5 - 0 0 3 8 - PREPAR: ACTUAL R E L D A T E R E L D A T E PANEL MO DA YR MO DA YR CODE A PHY I C D APS MODULES ON L A U VEH/SAT ICD-CCBD IRN-CCBD IRM-CCBD I0 ' 201-66-143 201-66-0239 201-66-0234 A PIPING CRITERIA S-IVB ICD-CCBD 2 0 1 - 6 6 - 0 1 0 8 IRN-CCBD 2 0 1 - 6 6 - 0 3 0 5 APS PNEU U N I T S / I B 11-10-65 LO-FA 040-347 HSFC-EC �. APOLLO INTERFACE CONTROL DOCUMENT LOG PAGE 10 DATE 2 9 J U L 66 -- -- --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUM8ER ------------------- --- ....................................... 50ML2614 - DEF SAT I B SRSC TEST ENCOD/LC-34+LC-37 50M12621 - DEF SRSC DECODER/LC-34 + LC-37 I N T F - 50M12622 503.112623 50M36801 65 1 6 0 5 3 6 8 .. - - - SCHED ACTUAL REL DATE R E t ' DATE PANEL MO D h YR MO DA YR CODE -------- -------- ------ PREPARING INTERFACE AREAS CENTER OR C E I N U M B E R S ACT ITY - --------- I - 07-1 5 - 6 6 IC 280-290 MSFC-ASTR 07-15-66 IC 280-290 MSFC-ASTR 07-1 5-66 IC SEE-DUG MSFC-ASTR 03-15-66 M-NF 040-090 MSFC-M-ED 09-14-65 LOPG 100-230 KSC-EDV 100-230 KSC-EDV 100-230 KSC-EDV DEF S A T I B SRSC I N D PANEL/LC-34+LC-37 DEF SAT 1 8 SRSC CODE PLUG/DECODER IMTF I C D SATURN I B / V CONTROL RATE GYRO PKG P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED FLD SYS L C 3 4 SS FUNC I N T F REQMTS GHE L C 3 4 S/C GSE 09-15-65 LOPG FUNC I N T F REQMTS GN2 L C 3 4 S/C NO IRN-CCBD ENTERED GSE 09-1 5 - 6 5 LOPG 09-15-65 LOPG 100-230 KSC-EDV 04-05-66 LOFC 230-340 KSC-EDV 09-1 5-65 LOFA 230-340 KSC-EDV FUNC I N T F REQflTS GOX L C 3 4 S / C GSE A L C - 3 4 INTERFACE S / C GSE TO UMB TMR NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 4 UT P I P C R I T NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD + I N T F LOC S / C F L D SYS - ENTERED ENTERED ENTERED A L Y ESE TO F A C I L I T Y C A B L I N G L C - 3 4 ICD-CCBD 201-66-0344 10-06-65 LO-EL 220-340 MSFC-ASTR �IA01 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 : .. DATE " 2 9 J U L 6 6 H D G S -- DOCUMENTNUMBER, DR R E V I S I O N NOTICE DOC REV . .. . AS 507 DOCUMENT T I T L E OR CCBD NUMBER CONT. ---- . . PAG SCHED ACTUAL R E L DATE REL DATE PANEL MO DA YR MO DA YR CODE PREPA I N T E R F A C E A R E A S CENTE ACT I V OR C E I NUMBERS -------- -------- ------ --------------- -----. , , , , , , , , , , , , , , ----------------------,-,,,,-------, - - FUNCT I N T F REOS ECS L C 3 9 PAD A S/C-GSE NO IRN-CCBD ENTERED 03-19-65 LOPG - F U N C T c I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG KSC-E - FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG KSC-K* 02-09-66 LOPG KSC-Ei 02-1 0-66 L /-FC KSC 03-19-65 LOPG KSC-K- 11-05-64 LO-FC MSC-N4 - L C 3 9 A S / C GSE FUNC I N T F LC-39 REQvGOX PAD B S / C FUNCT I N T F REQS ECS LC39 PAD 0 S/C-GSE B L C 3 9 L U T GSE SYSTEMS AFRM C O N F I G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - L C 3 9 A ML P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTEREL? FL SYS �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 AS -- --- -- 1 j DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV - - PREPARING I N T E R F A C E AREAS CENTE' OR C E I N U M B E R S ACTIV.. E - -------- -------- ------ --------------- -------- ENTERED LOFA 230-390 KSC-DE L C 3 9 PHY I N T F C GOX COND PNL L E A K T S U N I T NO IRN-CCBD ENTERED 07-22-65 LOFA 230-390 KSC-EDV ACCESS ARM + SERV MODULE C A B L E REQMTS NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO I R N - C f B D ENTERED 09-22-65 LOFA 230-390 KSC-EDV LEM U M B I L I C A L AND T E S T CABLES F.OR L C 39 NO IRN-CCBD ENTERED 08-20-65 + 09-22-64 GSE CABLES-GAS LC/34/37/39 TIMING N I T SYS COUNTDOWN D I S T < , " \ LOFA 230-390 KSC-EDV i LO-FC 230-340 . POWER REC* + CONN 11-29-65 LOFC 230-347 KSC-EDV-2 FUNCT I N T F REQMTS ECS MC LEM S / C GSE 05-03-65 LOPG 230-300 KSC-K-DT LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 10-01-64 LOFA 230-340 NSC-F AmC- . 8 L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR HO DA YR CODE 11-17-64 LC39-LUT A S/C - --- PAGE 202 CONTm DOCUMENT T I T L E OR CCQD NUMBER NO IRN-CCBD - 507 ----- LC34/37/39 SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED CM.0 ,,VOD ACCESS ARM C A B L I N G . . . -d. ---< '135.. �IAGl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS DATE 29 J U L 66 -- --- -- ) 5 D O C U M E N T NUMBER9 DOC REV OR R E V I S I O N N O T I C E - .................... --- J 65iCD0304 DOCUMENT T I T L E OR CCBD NUMBER ---------------------------------ma----- - SCHED ACTUAL R E 1 DATE R E L DATE P A N E L MO DA YR MO DA YR CODE PREPAF I N T E R F A C E AREAS CENTEF OR C E I NUMBERS ACTIVI -------- -------- ------ --------------- ------ VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A MOCK-UP - PAGE CONT. c H G j--- \, 507 ----- 2 3 AFRM 9 T O ACCESS ARM MHT RM 11-18-64 LOFA 230-300 HSC-FC 03-1 7-65 LOFA 230-300 KSC-DE C / M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 HSC-EC P H Y I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER 12-1 0 - 6 5 LO-FA 110-300 KSC-EC SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC 220-390 MSFC L C 3 9 VAB H I G H BAYS TO L / V 11-1 9 - 6 5 LOFC 220-390 KSC-F LC 39 V A B LOW BAY AREA TO L / V - E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-EC: L C 3 9 MSS TO L / V ESE/GSE ICD-CC8D 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-EC L C - 3 9 PAD AREA L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-EC S - I C / M L HOLD DOWN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC 220-390 MSFC - C 65ICD9200 ESE/GSE WIND LOAD A L L E V I A T I O N SYS F A C I L T O L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E E S E . ICD-CCBD 501-66-01243 * .. 09-0 1-66 03-09-66 LOFC 000-040 HSFC LO-EL 220-390 MS FC-L �APOLLO INTERFACE CONTROL DOCUMENT LOG D A T E 2 9 J U L 66 AS -- --- -- 3 S DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV 507 ----- IAOl CONT. P A G E 204 --- SCHED ACTUAL REL DATE REL DATE PANEL MU DA YR PI0 DA YR CODE DOCUMENT T l T L E OR CCBD NUMBER -------- ------- ------ PREPASTMG INTERFACE AREAS CENTE OR CEI N U M B E R S A C T l V f TY - , ------- ----------I--- IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED - 08-14-65 LOEL 02-1 1-66 LO-EL 02-11-66 LO-EL 02-1 1-46 LOEL 220-290 HSFC-ASTR ? - .LOW B A Y ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 HSFC i - LOW BAY E S E TO I N S T R SYS AND REC 1CD-CCBD 5 0 1 - 6 6 - 0 0 8 2 02-1 1-66 LO-EL 220-290 HSFC-ASTR S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD SO 1 - 6 6 - 0 0 3 2 'IRM-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRM-CCBD 5 0 1 - 6 6 - 0 0 3 2 '09-09-65 - L V ESE TO RANGE SEQUENCING LC-39 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 - - LICD-CCBD V ESE TO I N S T R SYSTEM 501-66-0084 IRN-CCBD IRN-CCBD - - 220-370 HSFC-ASTR , 501-66-0122 501-66-0265 MSFC COUNT CLOCK TO KSC T I M I N G LC-39 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED . L V ESE TO KSC DATA MEASUREMENTS . .. . . ,/ : 4 LOPG 250-390 MSFC-KSC , i ;-L �\ I ) PAGE DATE 2 9 JUL 66 -- )'C H G ; IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG --- D S --a -- DOCUMENTNUMBER9 OR R E V I S I O N N O T I C E DOCUMENT T I T L E OR CCBD NUMBER -------------------- --- ........................................ - FUNCT I N T F F L U I D REQMTS GHE SYS SAT - -------- .=---0--- --------------- ------ 0----- V 06-28-65 LOPG 010-250 KSC-P+ FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRM-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+ FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+ FUNCT INTF FLU1 G REQmTS ' L H 2 SYS 'SAT V NO IRN-CCBD ENTERED IRM-CCBD 50 1-66-0372 IRN-CC8D 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LaPG 010-250 KSC-P+ FUNCT I N T F F L U I D REQMTS L O X SYS SAT V I CD-CCBD 50 1-66-0040 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1-66-0040 06-03-65 LOPG 010-250 KSC-P+ FUNCT INTF F L U I D REQMTS R P - 1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CC.BD 5 0 1-66-004 1 06-15-65 LOPG 010-250 KSC-P+ 05-19-65 LOPG 000-260 -KSC-K- 02-08-66 LO-PG 220-390 MSFC-Ei NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVI SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO D A YR CODE DOC REV ENTERED ENTERED ENTERED SYS SAT V FUNCT I N T F F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED P I P C R I T APS PROP S E R V I C I N G SAT V 9. . " �APOLLO INTERFACE CONTROL DOCUMENT LOG AS DATE 2 9 JUL 66 -- --- -- DOCUMENT NUMBER, OR REVISION NOTICE .................... 507 ----- IhOl P A G E 2 0 6 ..-. CONT. DOC REV DOCUMENT TITLE OR C C B D NUMBER --- ...................................... --- ACTUAL SCHED RE1 DATE REL DATE PANEL MO DA YR MO DA YR CODE PREPARING INTERFACE AREAS CENTER OR C E I NUMBERS ACTIVET" ------. *- - -------- -------- ------ ------------- , , I I 7 ICD-CCBD 501-66-0150 - - - - -. UHB AND SERV CONN PLATE 3-4 S I C AFT ICD-CCBD 501-65-40 I RN-CCBD 50 1-66-0299 IRN-CCBD 501-66-0289 IRN-CCBD 501-66-0378 08-10-65 LO-FA 010-210 KSC-P+VE UMB + SERV CONNS PLATE N O 1-2 S-IC AFT ICD-CCBD 501-65-38 IRN-CC9D 501-66-0298 I RN-CCBD 50 1-66-0286 IRN-CC3D 501-66-0381 08-1 8-65 LO-FA 010-210 KSC-P+VE UMB + SERV CONNS PLATE NO 3-2 S-,IC AFT ICD-CCBD 501-65-39 IRN-CCBD 501-66-0282 IRN-CCBD 501-66-0382 . 08-10-65 LO-FA 010-210 MSFC-P+VE MOTION E N V AFT UMB PLATES l929+3 S-IC ICD-CCBD 50 1-66-0042 IRN-CCBD 501-66-0287 08-10-65 LO-FA 010-220 KSC-P+VE PHY ICD LAU VEH S-IC INTK UMB/LC39 GSE ICD-CCBD 501-65-36 IRN-CCBD 501-66-0290 IRN-CCBD 501-66-0296 I RN-CCBD 501-66-0378 08-09-65 LO-FA 010-390 KSC-P+"-' PHY ICD LAU VEH S-IC F W D UMBfLC39 GSE ICD-CCBD 501-65-37 IPM-CCBD 501-66-0190 08-09-65 LO-FA 010-390 KSC-P+VE (- -. ('- '. * .., <- 7. ,, ('; �IA 0 1 A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G \ , PAGE D A T E 2 9 JUL 66 -- --- -- C H G D DOCUMENT NUMBERS OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR C C B D NUMBER --- - -------------------- --- ....................................... SCHED ACTUAL R E L DATE R E L DATE PANEL MO D A YR MO D A YR CODE -------- ---e--- -----9 PREPAR l INTERFACE AREAS CENTER OR C E I NUMBERS ACTIVIl --------------- -------I IRN-CCBD 5 0 1 - 6 6 - 0 3 8 4 NO I R N - C C B D E N T E R E D J 65ICD9746 .+ o -S R R R R - 2 3 4 5 - - UMB + S'ERV CONNECTZONS S - 1 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 I RN-CCBD 50 1-66-01 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 I R N - C C B D 501-66-0295 I R N - C C B D 501-66-0383 INTERM 06-28-65 LO-FA 020-390 KSC-?+\ U M B I L I C A L -6 S E R V CONN S I I L O X D I S C O N N E C T ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 4 6 - 0 1 2 7 06-2 1 - 6 5 LO-FA 020-390 KSC-P+L U M B I L I C A L + S E R V CONN S - X I I C D - C C B D 501-66-0126 IRN-CCBD 5 0 1-66-0126 LH2 D I S C 06-21-65 LO-FA 020-390 KSC-P+L S-II FORWARD 06-28-65 LO-FA 020-390 KSC-P+V U M B I L I C A L 4 S E R V I C E CONN ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO TSY-CCPn E N T E R F n : t .r , : : ' ;.;--/,,,;:4cj . . : i !. I. 'T i11i;iS 5---IVIJ FGKWARD :, 7 . 7 , :.,,~j,-.!.~,.,-.', i-<~i-;'.i:~:i) : ! t l ~ - ( ~ / ~ - ~ ' ~ ~ ' t , ~ , �PAGE 208 DATE 2 9 J U L 66 -- D s _ -a- --- -- DUCUMtNT NUMBER, u k I~LVISION NOTICE DOC REV L O C U M ~ N I r I v t t UK C C B D NUMBER --__--- --- -.-----. ..".---.---..-.---.-. __._ . _ _ _ _ _ _ _ _ _ _ _ _ _ - SCHED ACTUAL REL DATE R E L DATE PANEL PI0 DA YR MO DA YR CODE -------- .--".--..-------.-I---.----- t I F i R 1 ~-'ICI.\L + S E % V I C F , CONNECT IOf~IS IU 1l ; ~ ~ - ~ ~512 ~ 1-;,5-->1: [ ; --.'77-r.--.-.- PREPARING INTERFACE AREAS CENTFQ OR C k I N U M B E R S ACT]. :Y - --- -...----------------- -----r----- 06-1 8-65 LO-FA 090-39.0 KSC-P+?E 0].-2H-oh LO-FA 020-390 KSC-P+VE 06-21-65 LO-FA . 220-390 KSC-P+VE >-J - 1 k!.!-l;l.&;l; :,i: l-,>l,-t.:; 1'.!1-4:t:?..,! 'let ;--,'!I>-I'';.:./~ pl..'1 ! r:t-. ~ ; K l ' iE i ? i r,')-ccPz 1 RN-CCSD - * , I . ' i, 5 ". --e'.i,-t.I c-!VFj CONS SET L C 3 9 PNEU Lq 50 1-66-0374 PHY I C D S - I V B ICD-CCBD HT EXCH DSV-48-438/SAT 50 1 - 6 6 - 0 1 0 4 V I J 651CD9759 - 1 65IC09761 PHY I C O I U COOLING U N I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 PHY I C D ICD-CCBD IRN-CCBD + P I P I N G CRIT IU PNEU CONS + P I P I N G C R I T E R I A 09-1 5 - 6 5 LO-FA 220-390 HSFC-EDV 09-1 5 - 6 5 LO-FA 220-390 MSFC-EpU 06-21-65 LO-FA 220-390 KSC-P+YE 09-1 5 - 6 5 LO-FA 220-390 MSFZ-ECV 501-65-48 5 0 1-66-0292 PHY I C D APS PNEU CONS DSV-48-436/SAT ICD-CCBD 50 1-66-0104 V - P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1-66-0314 - -PHY I C D S-IC INERT PREFILL + PIPING CRIT �A P O L L O I N T E R F A C E C O N T R O L DOCUMENT L O G DATE 29 JUL ,-- * --1c , H '\ 66 --- -- ACTUAL R E L DATE R E L DATE P A N E L MO DA YR NO D A YR CODE SCHED D S - , , , DOCUMENTNUMBERs DR R E V I S I O N N O T I C E ,,,-,.,,,,,,, , , , , , , - DOC REV ,-.,-.,-,.,._-- DOCUMENT T I T L E OR C C B D NUMBER , , , =-----7----= .3--------------- --PIC--.= ------I=-- -.=-----.- PREP CENT INTERFACE ARE4f OR C E I NUMBERS ACYI ._--.-- CI-.-.i-------c=--- L/ ICD-CCBD 4'7 r' J 65ZCD9762 - s I? R PHY I C D S - I 1 V PNEU CONSOLES S 7 - 4 f B i S A T 06-25-65 LO-FA 220-390 K3C- 06-25-65 LO-FA 220-35'0 KSC- 06-25-65 LO-FA 220-390 KSC--1 02-11-66 LO-FA 220-390 MSFC. I C D ~ C C B D 501-65-28 I R N - C C B D 501-66-0124 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 *, -J 501-65-47 1 2 - - * - PHY I C D S I T PNEU CONSOLE S7-41C/SAT I C D - C C B D 501-65-29 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 4 V P H Y I C D S I I P N E U CONS S 7 - 4 1 A + 4 1 D / S A Y ICD-CCbD 501-65-30 I R N - C C B D 501-66-0130 1RN-CCBD 50 1-66-0300 P H Y I C D HEAT E X C H A N G E R A 7 - 7 1 / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IR N - C C B D 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 I R N - C C B D 501-66-0327 V - V PNEU SYS/SATURN V SEE-DWG SEE B A S I C NUMBER FOR R E V I S I O N , T I T L E v E T C , PHYS I C D S - I C HYDRAULIC U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 P H Y 1CD S - I C P N E Y C O N S O L E R K S ' 1-2-3+4 02-10-66 LO-FA 220-390 KSC-i �APOLLO INTERFACE' CON'TROL DOCUMENT LOG DATE 2 9 J U L 66 -- --- D S - AS -- DOCUMZNT NUMBER* OR R E V I S I O N NOTICE ------.-------------- DOC REV 507 ----- CONT. DOCUMENT T I T L E OR CCBD NUMBER --- SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR HO DA YR CODE PREPARING I N T E R F A C E AREAS CENT" OR C E I NUMBERS A C T I . , T Y - ---------u--------------------------=>=--- -Y- ICD-CCBD - - 501-65-61 PHY I C D PNEU CONSOLES 5 9 6 ~ 79 8 S - I C ICD-CCBD 5 0 1 - 6 5 - 3 4 08-09-65 LO-FA 220-390 KSC-P+VE PHY I C D S - I C PNEU CHECKOUT RKS 1 - 2 - 3 9 4 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 MSFC-EDV PNEU CONSOLE SET 02-07-66 LO-FA .220-280 MSFC-P+V 12-09-65 LO-FA 210-390 KSC-EDV 02-07-66 LO-FA 010-390 MSFC-EDV 02-10-65 LO-FA 020-220 MSFC-EDV 02-1 0-66 LO-FA 010-220 MSFC-EDV PIPING CRITERIA S-IC ICD-CCBD 501-66-0046 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 A S - I 1 STAGE GSE PLACEMENT ON MBL LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 J 65ICD9773 PAGE 210 - 65ICD9776-001 P I P C R I T S-IC FLUSH ICD-CCBD 5 0 1 - 6 6 - 0 0 4 7 PHY I C D ICD-CCBD IRN-CCBD IRN-CCBD 4 PURGE U N I T SAT V + P I P E C R I T S I 1 L E A K DETECT SYS 501-66-0155 501-66-0264 501-66-0274 PHY I C D P I P E C R I T S I C FWD UMB SERV U N SV ICD-CCBD 5 0 1 - 6 6 - 0 1 8 0 SEE-DWG SEE B A S I C NUMBER FOR R E V I S I O N e T I T L E c E T C o - PHY I C D + P I P C R I T HAZ GAS ANALYZER SATV ICD-CCBD 5 0 1-66-0100 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 7 02-04-66 LO-FA 220-000 MSFC-EDV E �I A@\ A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G PAGE DATE 2 9 J u t 66 ' -- --- -- c H \ D DO CUM EN^ N U U B E R s OR R E V I S I O N N O T I C E G ___ _ ------ ---------.=---- DOC REV --- DOCUMENT T I T L E OR C C B D NUMBER ICD-CCBD - -2=-)-------------- U-.--_--O--U------------ -------.= - - - = - - - - - - C C C C C -----LO- CeCO-C U-,=CCC V 06-25-65 LO-FA 220-390 KSC- 06-25-65 LO-FA 220-390 KSC-P+' 06-25-65 LO-FA 220-390 KSC-P+' 06-25-65 LO-FA 220-390 KSC-'F+' 02-11-66 LO-FA 220-390 MSFC-E :) s- 501-66-0124 5 0 1-66-030 1 - P H Y IC3 SPE PNEU C O N S O L E S 7 - 4 1 C / S A T ECD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 I R N - C C B D 501-66-0294 - PHY I C D S Z i PNEU CONS S 7 - 4 P A + 4 1 D B S A T ICD-CCZD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 I R N - C C B D 501-66-0300 - PREPAP I N T E R F A C E ARE4S CENTER OR C E I NUMBERS tICTIvI 501-65-47 PHY I C D S - 1 1 PNEU CONSOLES S 7 - 4 1 B / S A T ZCD-CCBD 50 1-65-28 IRN-CCBD IRN-CCBD SCHED ACTUAL R E L DATE REC DATE PANEL MO D A Y R MO D A YR CODE PHY I C D HEAT EXCHANGER A ? - 7 P P S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 I RN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 V V - V - PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 IRN-CCBD 501-66-0327 * SEE B A S I C NUMBER FDR R E V I S I O N 9 T I T L E 9 E T C o PNEU S Y S / S A T U R N V SEE-DWG L . J 65ICD9768 - PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 PHY I C D S - I C PNEU C O N S O L E RKS 1-2-3+4 02-10-66 LO-FA 220-390 KSC-K-I 09-2 5 - 6 5 LO-FA 220-390 KSC-K-I �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G 7 D A T E 2 9 4UL ,-1 ?c : fi L 66 -- ---- -- -1 2 S OOCUMENT NUMEERc 3 R R E V I S I O N Ni3TICE DCC RE'd DOCURENT T I T L E O R G C R D NUMBER SCHED ACTUALREL D A T E R E L DATE PANEL MO D A Y R MO D A YE. CODE ---.= A --.r*.a --- -- -, .- -. PKEF INTF OR ' -...-. AREAS LExI 4fu3 r ~ r ; .. . - " i-1333,YJll F.kY L 3 C F C R T TU K A T E h A L C U M C A R T I C E - C C S D 5 0 1-66-0207 L2cc 2 3 0 - 39!1 hC1 01-20-66 LOFC 230-39C: K 5:- 11-01-66 FH 000-1 0:: U5'C. 02-05-66 -,'+++ -? b61CD7009 4 80M90507 - LC39 S / t D O C o POWER S U P P L l E S FLIGHT M E C H A N I C S P A N E L ICD : �APULL(T3 I N T E H F AC"E CONTROL DOCI.JMENT L O G D4Tt 0 S _ - PAGE 2 1 2 2 9 J U L 66 --. -.. . *-- - - DOCUMENT N U M B E R * DR R E V l S I O N N O T I C E -NU.*-.--. - -- DOC REV DOCUMENT T I T L E OR C C B D NUMBER .--.*-.-- -PI-->, ' - ...<-. li... ..>-i,-lrilC .. --.U. .-,I-, .C . ...:.---.---.-_F_C . . ir.2.:. .... .-.- .----- i . SCHED ACTUAL REL DATE R E L DATE PANEL MO D A Y R HO DA. YR CODE . .. = . .. . . . PREPARING , I N T E R F A C E AREAS C E N T E R OR CEE NUMBERS A C T Z V I T Y . . . - J . , .. --- . . L A U V E H P S P A C E C R A F ? PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 I RM-CCBD S O L - - 4 6 - - 0 1 9 8 LAU V E H / S P k C E C R A F % F U N C T I O N A L I C D - C C B D 50 1 - 6 6 - 0 3 3 5 REQ B ENVEL.OPE LEMBS-XVBB It! C L E A R A N C E P H Y S I C A L I C D - C C B D 501-66-0099 - I N S T R U M E N T U N I T T O S P A C E C R A F T PHYS REQ NO I R N - C C E O E N T E R E D IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 ZRN-CCBD 5 3 1 - 6 6 - 0 2 1 4 - - S P A C E C R A F T T O Q-BALL I C D - C C B D 501-66-0242 IRN-CCBD 50 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 P H Y S REQ B SATURNIAPOLLO FREQ PLAN ICD-CCBD - 05-1.0-66 IC 000-100 MSFC 08-06-65 C-S 000-100 MSFC 03-18-65 E I 300-230 MSC 08-12-65 E I 300-100 MSC 501-66-0256 EM1 C O M P A T I B l h I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 ! 0 D E S I G N C R I T E R I A FOR S A T U R N V ONBOARD EDS ICD-CCBD A 16331-63A107350 A 16331-63A107393 - 5 0 1-66-0078 E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 k SOFTWARE I C D - A C E COMP I N T F S/C-L/V COHP I N T E R F A C E .. �j A P O L L O I N T E R F A C E CONf ROL DOCUMENT L O G D A T E 2 9 JUL PAGt 66 -- --- -- ) )C H G )-" " D O C U M E N T NUMSERs OR R E V I S I O N N O T I C E DOC REV A 40M05486 - - - -, ACTUAL SCHED RED D A T E R E i D A T E P A N E L MO D A YR MO D A YR CODE DOCUMENT T I T L E OR C C B D NUMBER PREPAR I N T E R F A C E AREAS C E N T E R OR C E I NUMBERS ACTIVI -------- -------- ------ --------------- ------ ' '-'""--"'" " ' ' "-"-'---""---"-------------------'"-"-- ICD-CCBD j IAOI 501-66-0083 t V ESE/PROPELLANT SYSTEMS ICD-CCBD 501-66-0034 L V E S E TO L A U N C H E Q U I P M E N T ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 MSFC-A S P A C E C R A F T GSE TO L A U V E H GSE EI HSFC-A I N S T U N I T T O S P A C E C R A F T E L E C REQ EI MSFC-A Cs MSFC-A E D S CHECKOUT S C H E H A T I C S EI MSFC I C D S A T U R N I B / V CONTROL R A T E GYRO PKG M-NF MSFC-P 01-28-65 LOFC KSC-F L C 3 9 DATA TRANS S Y S ( W I D E BAND) NO I R N - C C B D E N T E R E D 02-02-65 LOFC KSC-F 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 -K S C 03-23-65 LOFC 230-390 KSC-F 0 3 - 1 5-65 LOFC 230-390 KSC-EC D E S OF SA.TURN S A - 5 0 8 + A P O L L O S C EDS L C 3 9 S I T E P L A N + GENL ARRANGE-SIC NO I R N - C C B D E N T E R E D A 65ICD7002 - L C 3 9 OPNL INTERCOM SYS-S/C 65ICD7003 - L C 3 9 FAC I N S T CABLING-LOC/ROUTING A 65 I C D 7 0 0 4 - L C 3 9 O P N L T V SYS-FAC-S/C E 65ICD7006 A L C 3 9 SAT V TRANSP 9OUTES -S/C GSE ESE/GSE ESE/GSE ' S/C �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 214r' DATk 2 9 JUL -- --- 66 --- -- DOCUMENT NUMBER* OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER ------------------- --- ........................................ 65 ICD7010 A . L C 3 9 SAT V VEH STAGE 4 S/C MISALIGNMENT SCHED ACTUAL R E L D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE 08-13-65 LOFC 04-2 8-65 LOFC ... PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I ' ! - 100-390 KSC-EDV-2 230-390 KSC-F -. ' - A L C 3 9 CSM + LEM TO F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRh-CCBD ENTERED NO IRN-CCOD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 65ICD7052 - S/C GSE TO HAZARD PROOF MON S Y S T v L C - 3 9 A L C 3 9 VAB H I G H BAY AREA TO S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - . - .--\ ..i 1 - \ FUNCT I N T F REQS ECS L C 3 9 V A B SIC-GSE 03-19-65 LOPG 100-390 KSC-K-DT \- 1 �1 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG I PAGE D A T E 2 9 J U L 66 -- --- -- I SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE C H O G - ,--I DOCUMENT NUMBER9 OR R E V I S I O N NOTICE A 65ICD7167 1 ; A 65ICD7300 R R R DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - FUNCT I N T F RQMTS ECS L C 3 9 / V A B LEM - 2 4 6 L C 3 9 LCC F A C I L I T Y S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED -------- -------- ------ ---------------SC GSE ESE/GSE F 65ICD7468 - LC39 PIPING NO IRN-CCBD NO IRN-CCBD NO IR.N-CCBD NO IRN-CCBD LC39/MSS C R I T + I N T F LOC S / C ENTERED ENTERED ENTERED ENTERED F L D SYS P I P C R I T + I N T F LOC L E H FLD' SYS L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD ENTERED ENTEREQ 05-03-65 LOPG 03-05-65 A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD- E;.ITERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - PREPAF I N T E R F A C E AREAS CENTEF OR C E I NUMBERS . A C T I V I me----- 230-390 KSC-K- 230-390 KSC-i 01-25-65 LOFC 230-390 KSC-F 09-03-65 LOPG 100-200 KSC 12-02-65 LOPG 140-390 01-12-65 LOFC 230-390 KSC-El * KSC-F �APOLLO I N T E R F A C E CONTROL DOCUMENT LO^ D A T E 29 j U L 66 PAGE 2 1 6 -- --- -- D S DOCUMFNT NUMBER, OR R E V I S I O N N O T I C E --- DOC REV - - SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA Y R M O D A YR CODE DOCUMENT T I T L E OR CCBD NUMBER - FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE NO IRM-CCBD ENTERED 03-19-65 FUNCT I N T F , R E Q M T S GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-EDV FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-K-DT L C 3 9 A S / C GSE FUNC I N T F REQvGOX 02-09-66 LOPG 230-390 KSC-EOV 02-10-66 L/-FC 230-300 KSC 03-19-65 LOPG 100-390 KSC-K-DT 11-05-64 LO-FC 230-390 HSC-NAA 230-390 KSC-EDV LC-39 PAD B S/C FUNCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE B L C 3 9 L U T GSE SYSTEMS AFRM C O N F l G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CC8D ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - PREPARING I N T E R F A C E AREAS CENTER OR CEI NUMBERS A C B I V ~ T Y L C 3 9 A ML P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED F L SYS LOPG 100-390 KSC-K-DT ., .. .4 - ,- �1 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl DATE 29 J U L 66 \ -- --- -- jc H G )--- DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E DOC -REV SCHED ACTUAL R E L D A T E R E L DATE PANEL NO DA YR HO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER -------- -------- - ------------------- -"- ........................................ R NO IRN-CCBD 5 - - 11-1 7 - 6 4 LOFA 230-390 KSC-DE L C 3 9 PHY I N T F C GOX COND PNL L E A K TS U N I T NO IRN-CCBD ENTERED 07-22-65 COFA 230-390 KSC-EC ACCESS A R M NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD 09-22-65 LOFA 230-390 KSC-EC 9 N I T SYS SERV MODULE C A B L E REQHTS ENTERED ENTERED ENTERED ENTERED LEM U M B I L I C A L AND T E S T CABLES FOR L C 39 NO IRN-CCBD ENTERED .* LC/34/37/39 T I M I N G + COUNTDOHN D I S T 09-22-64 LO-FC 230-340 A,C, + CONN 11-29-65 LOFC 230-347 KSC-ED 05-03-65 LOPG 230-300 KSC-K- SM SWG ARM UM8 D I S C A 1 4 0 1 9 ENTERED ENTERED 230-340 MSC-FO SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED 230-340 KSC-ED CMD MOD ACCESS ARM C A B L I N G 230-340 KSC-D POWER RECo FUNCT I N T F REQMTS ECS MC LEM S / C GSE LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 8 L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - -------- ---I--------- ENTERED ~~39-LUG T S E CABLES-GAS A S/C - --a=-- PREPAF I N T E R F A C E AREAS CENTEF OR C E I NUMBERS ACTIV: LC34/37/39 . �APOLLO 1NTERFAC.E CONTROL DOCUMENT LOG DATE 29 JUL 66 PAGE 21: -- --- -- D S DOCUMENT NUMBER^ OR RE?!ISION NOTICE -- DOC REV - DOCUMENT T I T L E OR CCBD NUMBER VERT STOP FOR L E S ACCESS ARM NO IRN-CCBD ENTERED NO IRN-CC8D ENTERED A MOCK-UP J 651CD8311 - E 651CD9020 E 65ICD9041 .- - - SCHED ACTUAL REL DATE R E L . D A T E PANEL MO DA YR MO DA YR CODE 23' AFRM 9 T O ACCESS ARM WHT RM PREPARING INTERFACE AREAS CENT'? OR C E I NUMBERS ACT, ,TY - 11-18-64 LOFA 230-300 MSC-FO 03-1 7 - 6 5 LOFA 230-300 KSC-DE C/M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA 100-300 MSC-EDV PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER 3.2-10-65 LO-FA 110-300 KSC-EDV SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1-65-52 02-02-66 LOFC 220-390 PfS FC L C 3 9 V A B H I G H BAYS T O L / V 11-19-65 LOFC 220-390 KSC-F" L C 39 V A 8 LOW BAY AREA TO L/V-ESE/GSE ICD-CCBD 5 0 1-66-0086 02-09-66 LO-FC , 220-390 KSC-EDY-2 L C 3 9 HSS TO L / V E S E I G S E ICD-CCBD 501-66-0110 02-14-66 LO-FC 220-390 KSC-EDV-2 L C - 3 9 PAD AREA L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 XSC-" S - I C / M L HOLD DOWN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC 220-390 HS FC LOFC 000-040 - MSFC LO-EL 220-390 MSFC-ASTR ESE/.GSE WIND LOAD A L L E V I A T I O N S Y S F A C I L TO L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E ESE ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 09-01-66 03-09-66 "1-2 . �J APOLLO I N T E R F A C E CONTROL DOCUMENT L O G 3 - 3c H I IA 0 1 DATE 2 9 J U L 6 6 -- --- -- D DOCUMENT NUMBERo i3R R E V I S I O N N O T I C E G I--- .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- --------------------------------------- SCHED ACTUAL R E L DATE REL DATE PANEL MO DA YR MO D A YR CODE -------- ------_------- PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV -----------OD- ----- IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 NO IRN-CCBD ENTERED A 65ICO920f -\ - d l R 1 - L V E S P T O RANGE SEQUENCING L C - 3 9 08-14-65 LOEL 220-390 MS FC- 02-1 1-66 LO-EL 220-370 MSFC-I L V ESE TO I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL 220-290 MSFC-I MSFC COUNT CLOCK TO KSC T I M I N G L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED 08-14-65 LOEL 200-390 MSFC-I L V ESE TO KSC DATA MEASUREMENTS 02-1 1-66 LOEL 220-290 MS FC-4 LOW B A Y ESE TO I N S T R U SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 MSFC 02-1 1-66 LO-EL 220-290 MSFC-4 09-09-65 LOPG 250-390 ICD-CCBD IRN-CCBD 501-65-83 50 1-65-83 L V ESE/60 AC POWER REQUIREMENTS 501-66-0174 501-66-0324 ICD-CCBD IRN-CCBD . A 651CD9400 - R -. R 1 2 - REC LOW B A Y ESE TO I N S T R SYS AND REC ICD-CCBD -j 4 501-66-0082 S E R V I C I N G REQMTS ECS SAT V L C 3 9 I CD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 MSFC-I I �APOLLO INTERFACE CONTROL DOCUMENT LOG DATE 29 JUL 66 AS -- --- -- U _ S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV 508 ----- DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ ------I------------- - - - - J 651609540 - IAOl CONT. SCHED ACTUAL REL DATE REL DATE PANEL MO DA YR MO D A YR CODE PREPARING INTERFACE AREAS CEN. . 08 C E I NUMBERS ACTIVITY - -------- ------- ------ --------------- ---PO---- FUNCT I N T F F L U I D REQHTS GHE SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTEREO NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT l N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS L H 2 SYS SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG 010-250 FUNCT I N T F F L U I D REQMTS LOX SYS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 06-03-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 1 06-15-65 LOPG 010-250 KSC-P+VE - , FUNCT I N T F F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED P I P C R I T APS PROP S E R V I C I N G SAT V KSC-P+VE -.. ,,. - 7 - .. , SYS SAT V . ,. .3*%. . * . 0::-19-65 LOP6 000-260 KSC-K-DT 02-08-66 LO-PG 220-390 HSFC-EDV . �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 2 9 JUL 1401 PAGE 66 -- --- -ACTUAL SCHED R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE C H G --- D DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E ------------------I- DOC REV -0- DOCUMENT T I T L E OR CCBD NUMBER ....................................... ICD-CCBD - J 65ICD9740 Q 3 t R R R 1 a 2 3 - - - ----------------- -----I PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVZ --------------- ------ 501-66-0150 UMB AND SERV CONN P L A T E 3-4 ICD-CCBD 5 0 1 - 6 5 - 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 S I C AFT 08-1 0-65 LO-FA 010-210 KSC-P+ UMB + SERV CONNS P L A T E NO 1 - 2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT 08-18-65 LO-FA 010-210 KSC-P+' UMB + SERV CONNS P L A T E NO 3 - 2 ICD-CCBD 5 0 1 - 6 5 - 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT 08-10-65 LO-FA 010-210 MSFC-P M O T I O N ENV AFT UMB P L A T E S 1 * 2 9 + 3 S - I C ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-10-65 LO-FA 010-210 KSC-P+' PHY I C D L A U VEH S - I C ICD-CCBD 5 0 1 - 6 5 - 3 6 IRN-CCBD 50 1 - 6 6 - 0 2 9 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 6 I'RN-CCBD 501-66-0378 I N T K UMB/LC39 08-09-65 LO-FA 010-390 KSC-P+' PHY I C D LAU VEH S - I C ICD-CCSD 5 0 1 - 6 5 - 3 7 IRN-CC8D 5 0 1 - 6 6 - 0 1 9 0 FWD U M B / L C 3 9 GSE GSE - . 08-09-65 LO-FA 010-390 KSC-P+\ �* A P O L L O I N T E R F A C E .CONTROL DOCUMENT LOG AS DATE 2 9 J U L 66 -- - -- -- D S - DOCUMENT NUMBER9 OR R E V I S I O N NOTICE -----------s---O--_- 508 .---""-- DOC REV ___ CON?, PAGE 2 2 2 --- . DOCUMENT T I T L E OR C C B D NUMBER ....................................... SCHED ACTUAL R E L D A T E R E C DATE PANEL NO DA Y R MO DA Y R CODE ------- ------- -us--- IRM-CCBD 501-66-0384 NO IRN-CCBD E N T E R E D - UWB 4 S E R V CONNECT I O N S S - I 1 ICD-CCBD 501-66-0111 IRN-CCBD 501-66-0111 I RM-CCSD 501-66-029 1 IRN-CCBD 501-66-0295 I RN-CCBD 501-66-0383 - - 06-28-65 LO-FA U M B I L I C A L + S E R V CONN S I I LOX D I S C O N N E C T ICD-CCBD 501-66-0127 I RN-CCBD 501-66-0127 06-22-65 LO-FA U M B I L I C A L + S E R V COMN S - I 1 ICD-CCBD 501-66-0126 IRN-CCBD 501-66-0126 06-21-65 LO-FA 06-28-65 LO-FA 06-21-65 LO-FA 06-18-65 LO-FA * LHZ.DISC U M B I L I C A L + S E R V I C E CONN S-I1 ICD-CCBD 501-66-0125 I RN-CCBD 501-66-0125 IRN-CCBD 501-66-0297 NO IRN-CCBD E N T E R E D UMB FORWARD + SERV CONNECTIONS S - I V B AFT ICD-CCBD I RN-CCBD IRN-CCBD - INTERM 50 1-66-0178 50 1-66-028 1 501-66-0288 U M B + S E R V I C E C ~ N N E C T I O N S S-IVS ICD-CCBD 501-66-0177 IRM-CCSD 501-66-0283 FORWARD ' P R E P A R IPlG I N T E R F A C E AREAS CENTER OR C E % NUMBERS ACTI';. -.Y -------------- ---- >-- �A P O L L O I N T E R F A C E CONTROL DOCUMENT DOG D A T E 2 9 J U L 66 3 -- --- -- DOCUMENT NUMBER, OK R E V I S I O N N O T I C E SCHED ACTUAL REL DATE R E 1 DATE PANEL MO D A YR MO D A YR CODE DOC REV DOCUMENT T I T L E OR C C B D NUMBER ----____----------- ........................................ ----_-----.-.----------- --------------- -0- U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 IRN-CGBD 5 0 1 - 6 6 - 0 2 8 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 4 - J 65ICD9760 R , 1 J 651CD9761 - - LO-FA 090-390 K SC-P, 06-21-65 LO-FA 220-390 KSC-K- PHY I C D S - I V B P N E U CONS O S V - 4 8 - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V 06-21-65 LO-FA 220-390 KSC-Pi PNEU CONS S E T L C 3 9 01-28-66 LO-FA 020-390 KSC-Pi 06-21-65 LO-FA 220-390 KSC-P+ PHY I C D I U C O O L I N G U N I T + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 09-15-65 LO-FA 220-390 MSFC-I PHY I C D I U P N E U CONS PIPING CRITERIA 09-15-65 LO-FA 220-390 MSFC-I V 06-21-65 LO-FA 220-390 -K S C - P i 02-1 0-66 LOFA 220-390 MSFC-E 09-1 5-65 LO-FA 220-390 MSFC-E PHY I C D S - I V B H T EXCH D S V - 4 8 - 4 3 8 / S A T I C D - C C B D 501-66-0106 ICD-CCBD t 0 6 - 1 8-65 V IRN-CCBD - c---- PHY I C D S - I V B PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 PIPING CRITERIA S-IVB ICD-CCBD 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1 - 6 6 - C 3 7 4 - PREPA I N T E R F A C E AREAS C E N T E OR C E I NUMBERS ACTIV 9 V 501-65-48 5 0 1-66-0292 PHY I C D APS P N E U CONS D S V - 4 8 - 4 3 6 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 P I P I N G C R I T E R I A APS P N E U CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 PHY ICD S - I C INERT PREFILL + P I P I N G CRIT �APOLLO INTERFAC.E DATE 2 9 J U L 6 6 AS -- --- -- D __ S DOCUYENT NUMBER? OR R E V I S I O N NOTICE CONTROL DOCUMENT DOC REV 508 CON?. ----- -------------------- --- ........................................ 6 5 1CD9766-003 + - PHY I C D ICD-CCBD IRN-CCBD IRN-CCBD PAGE 2 2 -- SCHED ACTUAL R E L D A T E R E L . DATE P A N E L PI0 D A Y R MO 0 8 YR CODE DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD LOG -------- ----em- ------ PREPARING - I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT* '1TY 501-65-47 S-II PNEU CONSOLES S 7 - 4 1 B / S A T V 06-25-65 LO-FA 06-25-65 LO-FA 06-25-65 LO-FA 501-65-28 501-66-0124 5 0 1-66-0301 PHY I C D S I I PNEU CONSOLE S 7 - 4 l C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 L A + 4 1 O / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 5 0 1-66-0300 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 IRN-CCSD 5 0 1 - 6 6 - 0 3 2 7 V V V PNEU SYS/SATURM V KSC-P+VE - -4.. 06-25-65 LO-FA 220-390 KSC-+;YE 0 2 - 1 1-66 LO-FA 220-390 MSFC-EDV SEE-DWG SEE B A S I C NUMBER FOR R E V I S I O N I T I T L E VE f C . PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 220-390 02-10-66 LO-FA 220-390 KS C~K-0'1. . .. J 65ICD9768 .- PHY I C D S - I C PNEU CONSOLE RKS 1 - 2 - 3 + 4 09-1 5 - 6 5 LO-FA 220-390 . . KSC-K-DT . - �A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G PAGl D A T E 2 9 J U L 66 -- --- -- IC H D G $ COCUMENT NUMBER7 OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR C C B D NUMBER ....................................... ICD-CCBD - 65ICD9776-001 ', J 651CD9779 -.* *, R 3 PREPAI I N T E R F A C E AREAS C E N T E I OR C E I NUMBERS ACTIV 501-65-61 PHY I C D P N E U CONSOLES 5 9 6 9 7 + 8 S - I C ICD-CCBD 5 0 1 - 6 5 - 3 4 08-09-65 LO-FA 220-390 KSC-Pi P H Y I C D S - I C P N E U CHECKOUT RKS 1-2-344 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 HSFC-E PIPING CRITERIA S-IC ICD-CCBD 5 0 1 - 6 6 - 0 0 4 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 220-280 MSFC-F P N E U CONSOLE S E T A 5 - 1 I STAGE GSE P L A C E M E N T ON M B L LAUNCHER ICD-CC~D 501-66-0129 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 12-09-65 LO-FA - P I P C R I T S - I C F L U S H + PURGE U N I T S A T V I C D - C C B D 5 0 1-66-0047 02-07-66 LO-FA 010-390 MSFC-E 02-10-65 LO-FA 020-220 MSFC-f 02-10-66 LO-FA SEE-DWG - 220-000 MSFC-E - -. SCHED ACTUAL REL DATE REL DATE PANEL MO D A YR MO D A YR CODE PHY I C D ICD-CCBD IRN-CCBD IRN-CCBD + PIPE C R I T S I X L E A K DETECT SYS 50 1-66-0155 501-66-0264 501-66-0274 - P H Y I C D P I P E C R I T S I C FWD U M 8 S E R V U N SV ICD-CCBD 5 0 1 - 6 6 - 0 1 8 0 * SEE B A S I C NUMBER F O R R E V I S I O N p T I T L E I E T C a - PHY I C D ICD-CCBD IRN-CCBD + P I P C R I T HAZ GAS ANALYZER S A T V 501-66-0100 5 0 1-66-0377 4 02-04-66 LO-FA �v APOLLO INTERFACE CONTROL DOCUMENT L O G IAOl PAGE 22t D A T E 29 JUL 66 -- --- -- D S __ DOCUSVENT NUMBER9 OR R E V I S I O N NOTICE --. DOC REV DOCUMENT T I T L E OR CCBD NUMBER __--_--------------- ....................................... -s- R IRN-CCBD 4 SCHED ACTUAL REL DATE R E L ' D A T E PANEL MO DA YR MO DA Y R CODE -------- ----s-- PREPARf NG INTERFACE AREAS CENTER OR C E I NUMBERS A C T " " T Y --- ------ --------------- -- 501-66-0315 %- - L C 3 9 S/C D.C. - F L I G H T MECHANICS PANEL I C D LC-39 ' r LO-FA 220-390 KSC-EDV 02-08-66 LOFC 230-390 KSC - 01-20-66 LOFC 230-390 KSC-EDY-2 09-09-99 FH 000-100 HSFC-AERO HAZARD PROOF1 NG-S/C POWER S U P P L I E S ' 03-02-66 A L C 3 9 M L PHY LOC PORT I U WATER ACCUM CART ICD-CCBD 5 0 1 - 6 6 - 0 2 0 7 . �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 ) ) PAGE DATE 2 9 J U L 66 -- --- -- C H t3 G S --- DOCUMENT NUMBER? OR R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER -----------_------- --- ........................................ ) I ' + A 13M07083 D 13M50123 PREPAR I N T E R F A C E AREAS C E Y T E R OR C E I NUMBERS ACTIVI -------- -------- ------ ------------ ---c-- L A U VEH/SPACECRAFT PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 9 8 10-07-65 MI 000-1 0 0 HS FC- P L A U VEH/SPACECRAFT F U N C T I O N A L REQ ICD-CCBD 5 0 1 - 6 6 - 0 3 3 5 12-14-65 MI 000-100 MS FC- P 07-07-65 MI 000-100 MS FC-P 05-03-65 MP 000-100 NSFC-P B SATURN/APOLLO FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 2 5 6 05-10-66 IC 000-100 MSFC - 08-17-65 IC 000-100 MSFC-I 08-06-65 C-S 000-100 PlSFC 03-18-65 EI 300-230 -HSC 08-12-65 EX 300-100 MSC - B ENVELOPE L E M I S - I V B / I U ICD-CCBD - CLEARANCE P H Y S I C A L 501-66-0099 INSTRUMENT U N I T TO SPACECRAFT PHYS REQ NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 PHYS REQ EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A ICD-CCBD 2 0 1 - 6 6 - 0 1 1 4 8 DESIGN CRITERIA FOR S A T U R N ICD-CCBD 5 0 1 - 6 6 - 0 0 7 8 A 16331-63A107350 SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE - E L E C I C D ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 v ONBOARD EDS COMP I N T F �APOLLO I N T E R F A C E CONTROL DOCUMENT DATE 29 J U L 66 -- O S -.-- AS -- DOCUMENT NUMBER9 OR R E V I S I O N N O T I C E - ------------------- DOC REV -u- A 40M05488 R - 2.4 40M05532 - -------- ---Pa--- .ISc-=ES---. PREPARING I N T E R F A C E AREAS CENTER ACTIV'TY OR C E I NUMBERS - ----- --=------Q-------- .--- L V ESE/PRO,PELLANT SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 220-210 HSFC-ASTR L V E S E TO LAUNCH EQUIPMENT ICD-CCBD 501-65-86 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 220-210 HSFC-ASTR SPACECRAFT GSE TO LAUNCH V E H I C L E GSE 04-01-67 EI 220-230 WSFC-ASTR I M S T U N I T T O SPACECRAFT E L E C REQ 03-01-67 €1 000-100 HSFC-ASTR 09-04-67 CS 000-100 WS FC-AST C - I C D SATURN XB/V + APOLLO SC EDS -.. CONTROL R A T E GYRO PKG L C 3 9 S I T E P L A N + GENL ARRANGE-S/C NO IRN-CCBD ENTERED - LNOC 3 IRN-CCBD 9 D A T A TRANS S Y S f W I D E ENTERED - --- 501-66-0083 DES OF SATURN S A - 5 0 9 - PAGE 2 2 8 SCHED ACTUAL R E L D A T E R E L DATE PANEL HO DA YR MO D A YR CODE .~-m-u--oocxlo-o--D----.DO-.DD----le-Po--o-rrscr - IAOl CONT- DOCUMENT T I T L E OR CCBD NUMBER ICD-CCBD .a 509 --.--- LO^ L C 3 9 OPNL I N T E R C O H SYS-S/C GSE BAND) ESE/GSE L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G S/C 230-390 KSC-F 01-28-65 LOFC 02-02-65 LOFC 230-390 KSC-F 02-06-65 LOFC 230-390 KSC-T 02-08-66 LOFC 230-390 KSC t . . .. - 02-23-65 LOFC 230-390 KSC-F A L C 3 9 SAT V TRANSP ROUTES - S I C 03-1 5-65 LOFC 230-390 KSC-EDV-2 A L C 3 9 SAT V VEH STAGE + S / C M I S A L I G N M E N T 08-13-65 LOFC 100-390 KSC-EDV-2 L C 3 9 OPNL T V SYS-FAC-SIC ESE/GSE R �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG -\ _ , DATE 2 9 J U L 66 AS I' c'/' H G D DOCUMENT NUMBER9 5% R E V I S I O N NOTICE DOC REV 509 PAGE CONTo DOCUMENT T I T L E OR CCBD NUMBER - - A L C 3 9 CSM o L E M T O F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED -. A 65 ICD7052 - S/C GSE TO HAZARD PROOF MON S Y S T p L C - 3 9 A L C 3 9 VAB H I G H B A Y AREA T O S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - - PREPAP I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVl SCHED ACTUAL R E L D A T E REE DATE PANEL MO DA YR MO DA YR CODE FUNCT I N T F REQS ECS L C 3 9 V A 8 S/C-GSE - - - - - - - --- - - 08--24-65 LOEL 230-390 KSC-VC 02-08-66 LOEL 230-390 KSC-L\ 04-28-65 LOFC 230-390 KSC-F 03-19-65 LOPG 100-390 KSC-K. 05-03-65 LOPG 230-390 KSC-K. ' , FUNCT I N T F RQMTS E ~ LS C 3 9 / V A B LEM SC GSE �IAOI APOLLO I N T E R F A C E CONTROL DOCUMENT L O G P A G E 230 DATE 2 9 J U L 66 --- --- .. D _S DOCUMENTNUMBERv OR R E V I S I O N N O T I C E - --,---- A 65fCD7300 . R 2 R 4 R 6 --- .".- *,w-O DOC REV __U - DOCUMENT T I T L E OR CCBD NUMBER P-Q-OOO---O-P-QP_0-0C -0-.=---T-- , . . . I E.C.L..*C.-VUOO~O L C 3 9 LCC F A C I L I T Y SEC ESECGSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-GCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - F 65ICD7468 A 65ICD7566 - LC39 P I P I N G NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD LC39/MSS C R I T + XNTF LOC S I C F L D SYS ENTERED ENTERED ENTERED ENTERED P I P CRIT L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD 9 I N T F LOC LEM F L D S Y S SCHED ACTUAL R E L D A T E R E h D A T E PANEL HO DA YR MO D A YR CODE UC)QC.L,CIOL. LI-EIDC,li.e.i,C. L - . - . l - . - S . - . 0 3 - - 0 5-365 PREPARING I N T E R F A C E AREAS CENTF" OR C E I NUMBERS A C T I \ . Y - . -OCC.-O--_)-)L3-.=-- L i . . ? , - 230-390 KSC-F 230-330 KSC-F 01-25-65 LOFC 09-03-65 LOPG 12-02-65 LOPG 140-390 KSC-EDV C A-12-65 LOFC 230-390 KSC-F 03-19-65 LOPG 100-390 KSC-K-DT ENTERED ENTERED FUNCT I N T F REQS ECS L C 3 9 PAD A S/C-GSE �IA O . APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 66 r' -- --- -- i/ <I 3C D S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -------------------- --- --------------------------------------- .. J * C 65ICD7568 ------ --------------- REQMTS GHE L C 3 9 A S / C GSE 05.-02-66 LOPG 100-390 KSC-E FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-K- 02-09-66 LOPG 230-390 KSC-El 4 02-10-66 L/-FC 230-300 KSC 03-19-65 LOPG 100-390 KSC-K- 11-05-64 LO-FC 230-390 HSC-NI FUNCT INTF ----I ENTERED I C 65ICD7569 3 -------- PREPC I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV -...----- NO IRN-CCBD - SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR NO DA YR CODE 65 ICD7600 - L C 3 9 A S/C LC-39 G S E FUNC I N T F REQVGOX PAD B S / C FUNCT XNTF REQS ECS L C 3 9 PAD B S/C-GSE B L C 3 9 L U T GSE SYSTEMS AFRM C O N F I G NO fRN-CCBD ENTERED NO IRA-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - L C 3 9 A VHL P I P C R I T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED F L SYS �APOLLO I N T E R F A C E CONTROL. DOCUMENT LO^ PAGE 2 3 2 DATE 2 9 J U L 66 -.-. --..... --- -- D S _ DOCUMEYTNUMBERp OR R E V I S I O N NOTICE -..--- -.T*IC .-,_-.------- J 65XCDZ788 DOC REV ---C D Y C O - - C - . - . E L - J 65ICD7790 R 1A R 2 R 3 R 4 - A 65ICD8001 E 65ICD8032 A 651CD8200 DOCUMENT T I T L E OR CCBD NUMBER - I I C C . L I r - - C -. . . .- C-C ->. . ->. C &.._I-. .- <-- C.C.CS.ci.2 -.:..=I-_li.<ii.a. . --a F > . . = . . . . . L . . D PREPARING I N T E R F A C E AREAS CENTER OR C E I N U M B E R S ACTIVJTY - ...OY;.-riOUCE-F,--- OYI;I.=,". - -- L C 3 9 - - L U F GSE CABLES--GAS N T V S Y S 93-22-65 LOFA 230-390 KSC-EOV LEM UMBILICAL AND TEST CABLES FOR L C 39 NO IRN-CCBD ENTERED 08-20-65 LOFA 230-390 KSC-EDV LC/34/37/39 09-22-64 LO-FC 230-340 11-29-65 LOFC 05-03-65 LOPG 230-347 , 230-30(f 10-01-64 LOFA 230-340 HSC-@~-HJ 5 L C 3 9 P K Y ENTFC GOX CUND PNL L E A K NO IRN-CCBD ENTERED TS U N F T ACCESS ARM + SERV MODULE CABLE REPMT5 NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBU ENTERED NO IRN--CCBD ENTERED A S/C - C=.. SCHED ACTUAL REC D A T E R E L D A T E PANEL MO DA V R MO D A VR CODE A-C, T I M I N G + COUNTDOWN D L S f POWER RECo 4 CONN FUNCT I N T F REQMTS ECS MC LEM S I C GSE LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD B L C 3 7 / 3 9 LEM NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD J 65ICD8302 - J 65 1CD8303 --VERT LC34/37/39 SM SWG ARM UMB DlSC A 1 4 0 L 9 ENTERED ENTERED KSC-EDV-2 - , KSC-K-DT SHG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED ENTERED ENTERED CMD MOD ACCESS ARM C A B L I N G STOP FOR L E S ACCESS ARM .11-17-64 LOFA 230-340 KSC-D 12-18-64 LOFA 230-300 XSC-FO - - �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG DATE 29 J U L 6 6 -- --- -- y c H 7G D S DOCUMENT NUMBER, O R R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBD NUMBER NO IRN-CCBD NO IRN-CCBD A MOCK-UP - - ENTERED ENTERED SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR M O DA YR CODE * 2 3 AFRM 9 TO ACCESS ARM WHT RM PREP I N T E R F A C E AREAS CENT OR C E I NlJMBERS ACTI' . 03-1 7-65 LOFA 230-30C: KSC-C I N T F REQ 11-04-65 LOFA 100-3.39 MSC-E COVER' 12-10-65 LO-FA 110-330 KSC-E SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC 220-390 MS FC L C 3 9 VAB H I G H BAYS TO L / V 11-19-65 LOFC 220-390 K S C-F C/M ACCESS ARM ADPT HOOD TO S / C PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 ESE/GSE - LC 39 VAB LOW BAY AREA TO L / V - E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC 220-390 KSC-E - L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-E - L C - 3 9 PAD AREA L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC 220-390 KSC-E - S - I C / M L HOLD DOWN ARMS P H Y S I C A L R E Q M T S ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC 220-390 MSFC LOFC 000-040 - MSFC LO-EL 220-390 MS FC- - WIND LOAD A L L E V I A T I O N S Y S F A C I L TO L / V A F A C I L I T Y CABLES FOR LAUNCH V E H I C L E E S E ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 . 03-09-66 �A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G P A G E ;'3& DATE 2 9 J U L 66 -- D -...- DOCUMEVT N U M B E R * OK R E V I S I O N N O T I C E _ ____________ S -- --- DOC REV DOCUMENT T I T L E OR C C B D NUMBER ---- --- ....................................... NO I R N - C C B D - - - -------- ------- ------ PREPAR I'iG I N T E R F A C E A R E A S CENTER OR C E I NUMBERS A C T I V ! T V - I - -- ----I ENTERED L V E S E T O RANGE S E Q U E N C I N G L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 L V E S E f 6 0 AC POWER R E Q U I R E M E N T S ICD-CCBD 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 02-11-66 LO-EL 220-370 MSFC-ASTY L V E S E TO I N S T R S Y S T E M ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL 220-290 MSFC-ASTR MSFC COUNT CLOCK T O K S C T I M I N G CC-39 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO I R N - C C B D E N T E R E D 08-14-65 LOEL 200-390 MSFC-ASTR L V E S E TO K S C D A T A MEASUREMENTS 02-11-66 LOEL 220-290 MSFC-ASTR LOW B A Y ESE TO I N S T R U S Y S + R E C ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL 220-290 PSFC LOW B A Y ESE TO I N S T R S Y S AND REC 0 2 - 1 1-66 LO-EL 220-290 KSFC- S E R V I C I N G REQMTS ECS S A T V L C 3 9 ICD-CCRD 5 0 1 - 6 6 - 0 0 3 2 IKN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSFC-KSC .. F U N C T I N T F F L U I D REQMTS GHE S Y S S A T V 06-28-65 LOPG 010-250 KSC-P+VE ICD-CCBD - SCHED ACTUAL REL DATE R E L DATE PANEL MO DA YR MO D A YR CODE I TR 5 0 1-66-0082 �1 , I . DATE 2 9 Jut APOLLO I N T E R F A C E CONTROL DOCUMENT LOG PAGE 66 -- --- -- C H G DOCUMENT NUMBER, OR R E V I S I O N N O T I C E --- -5 .................... I R R R j A 65ICD9402 R R 1 R DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD I 2 3 - 1 2 3 - - SCHED ACTUAL R E L DATE R E t DATE PANEL MD DA YR MO DA YR CODE -------- -------- ------ PREPAR 1 INTER'ACE AREAS CENTER OR C E I NUMBERS ACTIVIl ------- ------.--------- ENTERED ENTERED ENTERED FUNCT I N T F F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+\ FUNCT I N T F F L U I D REQMTS GHZ SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-?+\ FUNCT I N T F F L U I D REQMTS LH2 SYS SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG 010-250 KSC-P+\ FUNCT I N T F F L U I D REQMTS LOX SYS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 06-03-65 LOPG 010-250 FUNCT XNTF F L U I D REQMTS R P - 1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 1 06-1 5 - 6 5 LOPG 010-250 KSC-P+\ FUNCT I N T F F L U I D REQMTS V A B ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED 05-1 9-65 LOPG 000-260 KSC-K-I P I P C R I T APS PROP S e R V I C I N G SAT V ICD-CCHD 5 0 1 - 6 6 - 0 1 5 0 02-08-66 LO-PG 220-390 MSFC-EI SYS SAT V ,- KSC-P+\ �A P O L L O I N T E H F A C F CflNTRO!. AS D A T t 2 9 JUL 66 -- --- -- 3 5 OOCUMENTNUMBEK~ 3 2 R t V I S T U N NOTICE J 65ICC%j740 s 9 1 7 P 3 DOC REV - - - - - 509 ----- CQNT. SCHED ACTUAL REL DATE R E L DATE PANEL M O D A YR MO D A YR CODE PREPARING I N T E R F A C E AREAS CENT" OR C f I NUMBERS A C T I , TY -------- -------- ------ --------------- ---------- D O C U P E N T T I T L E OR C C B D NUMBER UMB AND S E R V C U N N P L A T E 3-4 ICD-CCHD 5 0 1 - 6 5 - 4 0 IKN-CCRD 5 6 1 - 6 6 - 0 2 9 9 IRN-CCDD 5 0 1 - 6 6 - 0 2 8 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 DOCUMENT L O G S I C AFT 08-10-65 LO-FA 010-210 KSC-P+VE UMB + S E R V CONNS P L A T E NO 1-2 ICD-CCBD 5 0 1 - 6 5 - 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT 08-18-65 LO-FA 010-210 KSC-P+VE UMB + S E R V C O N N S P L A T E NO 3-2 ICD-CCBD 5 0 1 - 6 5 - 3 9 IRN-CCBD 50 1-66-0282 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT 08-10-65 LO-FA 010-210 MSFC-P+V E , M O T I O N ENV A F T UMB P L A T E S 1 p 2 9 + 3 S - I C ICD-CCBD 50 1-66-0042 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-1 0-65 LO-FA 010-210 KSC-P+VE P H Y TCD L A U VEH S - I C ICD-CCHO 5 0 1 - 6 5 - 3 6 IRN-CCHD 5 0 1 - 6 6 - 0 2 9 0 IKN-CCGD 5 0 1 - 6 6 - 0 2 9 6 IR N - C C B D 501-66-0378 INTK UMB/LC39 08-09-65 LO-FA 010-390 KSC-P+VE ICD L A U V E H S - I C ICD-CCRD 5 0 1 - 6 5 - 3 7 I K N - C C P D 501-66-0190 IRN-CCEG 5 0 1 - 6 6 - 0 3 8 4 NO I R N - C C h D E R T E R E D FWD U M R / L c 3 9 08-09-65 LO-FA 010-390 KSC-~+V~? PHY GSE GSE �1 APOLLO I N T E R F A C E CONT R o t DOCUMENT LOG IAOl PAGE DATE 29 J U L 6 6 j -- --- -- )C H O G - )--- DOCUMENT NUMBER, OR R E V I S I O N N O T I C E --------------me---- DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ - UMB + SERV CONNECTIONS S - 1 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 I RN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 3 INTERM SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE PREPAR I N T S F Z A C E AREAS CENTER OR C E I NUMBERS ACTIVI -------- -------- ------ --------------- -----06-28-65 LO-F A G23-390 KSC-P+ - U M B I L I C A L + SERV CONN S I I LOX DISCONNEC'T ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-2 1 - 6 5 LO-F A 02'3-390 KSC-P+ - U M B I L I C A L + SERV CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 6 06-21-65 LO-FA 020-390 KSC-P+ - U M B I L I C A L + S E R V I C E CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED 06-28-65 LO-FA 020-390 KSC-P+ 06-1 8 - 6 5 LO-FA 040-390 KSC-P+ - - LH2 DISC UMB + S E R V CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 8 FORWARD AFT UMB + S E R V I C E CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 3 FORWARD U M B I L I C A L + S E R V I C E CONNECTIONS XU ICD-CCBD 5 0 1 - 6 5 - 3 5 * 06-18-65 LO-FA 090-390 KSC-P+ �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG AS DATE 2 9 J U L 66 -- --- -- O S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DDC REV 509 - --- SCHED ACTUAL REL DATE REC DATE PANEL MO DA YR M O DA YR CODE PREPARING I N T E R F A C E AREAS C E N T F OR C E I NUMBERS ACTIL- .Y -------- -------- ------ --------------- ---------- DOCUMENT T I T L E OR CCBD NUMBER - --------------------- --- ........................................ IRN-CCBD IRN-CCRD PAGE 2 3 8 CONT. ----- 5 0 1-66-0285 501-66-0284 PHY I C D S - I V B PNEU CONS DSV-4B-432/SAT ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 V 06-21-65 LO-FA 220-390 K S C-K- DT PHY I C D S - I V B PNEU CONS D S V - 4 0 - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V 06-21-65 LO-FA 220-390 KSC-P+VE PNEU CONS SET L C 3 9 01-28-66 LO-FA 0 2 0-390 KSC-P+VE 06-22-65 LO-FA 220-390 KSC-P+VE PHY I C D I U C O O L I N G U N I T + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 09-15-65 LO-FA '220-390 MSFC-EDV PHY I C D I U PNEU CONS + P I P I N G C R I T E R I A ICD-CCBD 5 0 1 - 6 5 - 4 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 2 09-1 5-65 LO-FA 220-390 MSFC-EDV - PHY I C D APS PNEU CONS D S V - 4 B - 4 3 6 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 4 06-21-65 LO-FA 220-390 KSC-P+VE - P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 50 1 - 6 6 - 0 3 1 4 02-1 0-66 COFA 220-390 FS FC-E DV --PHY I C D S-IC INERT P R E F I L L + P I P I N G C U I T ICD-CCBD 5 0 1 - 6 5 - 4 7 09-1 5-65 LO-FA 220-390 HSFC-EDV - P I P I N G CRITERIA S-IVB ICD-CCBD 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 4 PHY I C D S - I V B H T EXCH D S V - 4 8 - 4 3 $ / S A T ICD-CCBD 501-66-0106 V V �IAOl APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 DATE 2 9 J U L 6 6 AS 509 ACTUAL SCHED R E L D A T E R E t DATE PANEL MO DA YR MO DA YR CODE C . DOCUMENT NUMBER, H 7 G , OR R E V I S I O N NOTICE - J 65ICD9762 * R R 1 2 J 651CD9763 R * R DOC REV a - 2 3 65 I C D 9 7 6 6 - 0 0 3 * J 65ICD9767 - J 65ICD9768 - 3 65KD9769 - t DOCUMENT T I T L E OR CCBD NUMBER -------- -------- ------ PHY I C D S - I I ICD-CCBD IRN-CCBD IRN-CCBD PNEU CONSOLES S 7 - 4 1 B I S A T 501-65-28 501-66-0124 5 0 1-66-030 1 PHY I C D S I I PNEU' CONSOLE S 7 - 4 1 C / S A T ICD-CCBD 5 0 1 - 6 5 - 2 9 IRN-CCSD 5 0 1 - 6 6 - 0 1 2 8 I RN-CCBD 5 0 L - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 l D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T ICD-CCSD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 7 PAGf CONT. V V V V PNEU SYS/SATURN V PREPAf I N T E R F A C E AREAS CENTEI OR C E I NUMBERS ACTIV. ------ -----.-I--------- 06-25-65 LO-FA 220-390 KSC-Pd 06-25-65 LO-FA 220-390 KSC-Pi 06-25-65 LO-FA 06-25-65 LO-FA KSC-P. 02-11-66 LO-FA MSFC- SEE-DWG SEE B A S I C NUMBER FOR R E V I S I O N g T I T L E i ETC. PHYS I C D S-IC H Y D R A U L I C U N I T L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 1 8 3 02-1 0-66 LO-FA 220-390 PHY I C D S - I C PNEU CONSOLE RKS 1 - 2 - 3 + 4 ICD-CCBD 5 0 1 - 6 5 - 6 1 09-15-65 LO-FA 220-390 KSC-K 08-09-65 LO-F A. 220-390 K SC-P - KSC-K 4 PHY I C D '3NEU CONSOLES 5 , 8 1 7 + 8 S-IC �A P U L L O I N T F R F A C E CONTROt. DOCUMENT L U G DATE 2 9 J U L 66 -- --- -SCHED I D S __ _ DOCUMENT NUMBER, Dii REVISION NCTICE DOC REV DOCUMENT T I T L E OR C C B D NUMBER --- ........................................ ICD-CCBD - - - -------- -------- ------ --------------- -------a P H Y I C D 5 - I C PNEU CHECKOUT RKS 1-2-3+4 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 MSFC-ED! PIPING CRITERIA S-IC I C D - C C B D 5 0 1-66-0046 IRN-CCBD 50 1 - 6 6 - 0 3 0 6 02-07-66 LO-FA 220-280 MSFC-P+\ 12-09-65 LO-FA 210-390 KSC-EDV PNEU CONSOLE S E T - P I P C R I T - S - I C FLUSH I C D - C C B D 501-66-0047 - PHY I C D + P I P E C R I T S I I L E A K DETECT SYS TCD-CCBD 5 0 1 - 6 6 - 0 1 5 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 4 IRN-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-10-65 LO-FA 020-220 MSFC-ED\ - PHY I C D P I P E C R I T S I C F W D UMB SERV U N SV I C D - C C B D 501-66-0180 02-10-66 LO-FA 010-220 MSFC-ED\ + SEE 5.- C 3 3 7 8 0 MO D A YR MO D A YR CODE PREPARII I N T E R F A C E AREAS CF"'ER OR C E I NUMBERS AL .VIT' 501-65-34 A S - I 1 S T A G E GSE P L A C E M E N T ON M B L LAUNCHER IC-D-CCBD 5 0 1-66-0129 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 F ACTUAL R E L DATE R E L DATE P A N E L + P U R G E . U N I T SAT V SEE-DWG B A S I C NUMBER F O R R E V I S I O N V T I T L E I E T C - - PHY I C D + P I P C R I T H A Z GAS A N A L Y Z E R S A T V ICD-CCRD 5 0 1 - 6 6 - 0 1 0 0 IRN-CCRD 5 0 1 - 6 6 - 0 3 7 7 I RN-CCBO 50 1 - 6 6 - 0 3 1 5 02-04-66 LO-FA 220-000 MSfC-ED\ A L C 3 9 ML PHY LOC PORT I U WATER ACCUM CART 03-02-66 LO-FA 220-390 KSC-EDV �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 3 DATE 2 9 JUL 66 3c H G '-7 \/ D S DOCUMENTNUMBER, DR R E V I S I O N NOTICE --- - .................... DOC REV --- - ... 66ICD7007 661CD7009 - PREP1 I N T E R F A C E AREAS C E N T £ OR C E I NUMBERS ACT:\ ----'---'---"-------"""--"--""' ICD-CCBD J 3 +++ DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L DATE R E 1 DATE P A N E L MO DA YR MO D A YR CODE LC-39 501-66-0207 02-08-66 HAZARD PROOFING-S/C LOFC 230--390 KSC ~ ~ 3S 3 I C ' 0-C. POHER S U P P L I E S 01-20-66 LOFC 230-390 KSC-E F L I G H T MECHANICS PANEL I C D 09-09-99 FH 0 0 0 - 1 00 MS FC- �A P O L L O I N T E R F A C E ' CONTRO1. DOCUMENT LOG PAGE 2 4 2 D A T E 2 9 J U L 66 4- D S A DOCUMFNT N U M B E R t OR R E V I S I O N NCTICE --- DOC REV DOCUMENT T I T L E OR C C B D NUMBER --- ........................................ SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO D A YR CODE PREPARING I N T E R F A C E AREAS C E N T E R OR C E I NUMBERS ACT1 'Y -----------I---^--.-- 13M03083 R A --- -- - L A U V E H / S P A C E C R A F T PROCEDURAL REQ ICD-CCBD 5 0 1 - 6 5 - 7 7 I R N - C C B D 501-66-0198 - L A U V E H / S P A C E C R A F T F U N C T I O N A L REQ I C D - C C B D 501-66-0335 1 13M07083 O 13M50123 B E N V E L O P E L E M / S - I V B / I U C L E A R A N C E PHYS I C A L I C D - C C B D 501-66-0099 - I N S T R U M E N T U N I T T O S P A C E C R A F T P H Y S REQ NO I R N - C C B D E N T E R E D IRN-CCBD 5 0 1 - 6 6 - 0 3 8 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 1 4 SPACECRAFT TO Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 4 2 IRN-CCBD 5 0 1-66-0242 P H Y S REQ A S A T U R N / A P O L L O FREQ P L A N ICD-CCBD 5 0 1 - 6 6 - 0 1 3 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 8 - EM1 C O M P A T I B I L I T Y D E S I G N C R I T E R I A I C D - C C R D 201-66-0114 R D E S I G N C R I T E R I A FOR S A T U R N V ONBOARD EDS ICD-CCBD 4 16331-63A107350 - 08-17-65 IC 000-100 MSFC-ASTR 08-06-65 C-S 000-100 MSFC 03-18-65 E I 300-230 MSC 501-66-0078 E L E C I C D ACE S / , C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 5 COMP I N T F ' �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG IAOl PAGE DATE 29 J U L 66 -- --- -- 'C H D G DOCUMENT NUPI18ERI OR R E V I S I O N N O T I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER -------- -------- ------ -------------------- --- ....................................... --A 16331-63A107393 A SOFTWARE ICD-ACE S / C - L / V ICD-CCBD 5 0 1 - 6 6 - 0 0 8 3 R A 40#37526 A 40fl37564 ------. 393.-100 MSC L V ESELPROPELLANT SYSTEMS ICD-CCBD 5 0 1 - 6 6 - 0 0 3 4 12-15-65 E I 220-210 HSFC-A! - L V ESE TO LAUNCH EQUIPMENT ICD-CCBD 5 0 1 - 6 5 - 8 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 8 9 12-09-65 €1 220-2 10 MS FC-A! - SPACECRAFT GSE TO L A U V E H GSE EI 230-220 MSFC-A! I N S T U N I T TO SPACECRAFT E L E C REQ EI 000-100 MSFC-A! Cs 000-100 MS FC-A! M-NF 040-090 MSFC-M- 01-28-65 LOFC 230-390 KSC-F L C 3 9 DATA TRANS S Y S ( W 1 D E BAND) ENTERED 02-02-65 LOFC 230-390 KSC-F L C 3 9 OPNL I N T E R C O M SYS-S/C 02-06-65 LOFC 230-390 KSC-F 02-08-66 LOFC 230-390 KSC 03-23-65 LOFC 230-390 K-SC-F A L C 3 9 SAT V TRANSP ROUTES -S/C 03-1 5-65 LOFC 230-390 KSC-ED\ A L C 3 9 SAT V VEH STAGE + S / C 08-13-65 LOFC 100-390 KSC-ED\ 2A 40H05538 -----.---------- E I a A 40H05488 COMP I N T E R F A C E PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS. A C T I V I ' 08-12-65 - A 40H05486 4 SCHED ACTUAL R E L D A T E R E L DATE PANEL WO D A YR MO DA YR CODE - DES OF SATURN S A - 5 1 0 I C D SATURN I B / V + APOLLO SC EDS CONTROL R A T E GYRO ? K G L C 3 9 S I T E P L A N + GENL ARRANGE-S/C NO IRN-CCBD ENTERED GSE . NO IRM-CCBD - L C 3 9 FAC I N S T C A B L I N G - L O C / R O U T I N G - L C 3 9 OPNL T V SYS-FAC-S/C ESE/GSE S/C ESE/GSE MISALIGNMENT �APOLLO I N T E R F A C E CONTROL OOCUMENT LOG IAOl DATE 29 J U L 66 -- --- -- O S - DOCUMENT NUMBER* DR R E V I S I O N N O T I C E .................... DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ SCHED ACTUAL REL D A T E R E 1 D A T E P A N E L MO DA YR MO D A YR CODE PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT' TY - _------- ------- ------ --------------- ---------- A L C 3 9 CSM + LEM TO F A C I L I T Y CABLES NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED . NO IRN-CCBD ENTERED A 65ICD7052 - S/C GSE TO HAZARD PROOF MON SYST,LC-39 02-08-66 LOEL 04-28-65 - 230-390 KSC-LVO-2 LOFC 230-390 KSC-F r A L C 3 9 VAB H I G H BAY AREA TO S / C NO NO NO NO NO NO NO NO NO NO NO A 65 'CD7167 IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD IRN-CCBD ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED ENTERED - FUNCT I N T F REQS ECS L C 3 9 V A B S/C-GSE 03-19-65 LOPG 100-390 KSC-K-DI - FUNCT I N T F RQMTS ECS L C 3 9 / V A B 05-03-65 LOPG. 230-390 KSC-K-DT LEM SC GSE �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 DATE 29 J U L 66 PAGE -- --- -- 'c H G D DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV - DOCUMENT T I T L E OR CCBD NUMBER SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO D A YR CODE L C 3 9 LCC F A C I L I T Y S / C ESE/GSE NO IRN-CCBD ENTERED NO IRN-CC-BD ENTERED NO IRN-CCBD ENTERED PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS A C T I V I 03-05-65 230-390 KSC-F 01-25-65 LOFC 233-390 KSC-F 09-03-65 LOPG 100-200 KSC 12-02-65 LOPG 146-390 01-12-65 LOFC 230-390 -KSC-F 03-19-65 100-390 KSC-K-I 8 A L C 3 9 MAT-ESE/GSE NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO fRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - ' - ". - - LC39 PIPING NO 1RN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD C R I T + I N T F LOC S / C F L D SYS ENTERED ENTERED ENTERED ENTERED LC39/M.SS P I P C R I T + I N T F LOC LEM F L D SYS' L C 3 9 PAD A NO IRN-CCBD NO IRN-CCBD . ENTERED ENTERED . FUNCT I N T F REPS ECS L C 3 9 PAD A S/C-GSE LOPG ' KSC-ED' �APOLLO INTERFACE. CONTROL DOCUMENT LOG IA 0 1 PAGE 246 DATE 2 9 J U L 66 -- --- -- 0 S - DOCUMENT NUMBER, OK R E V I S I O N NOTICE --- DOC REV SCXED ACTUAL R E L D A T E R E L DATE PANEL MO DA Y R MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER 1 NO IRN-CCBD - -------- ------- ------ --------------- -- R PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACT!'."TY ---a --- ENTERED C 65ICD7567 - FUNCT I N T F REQMTS GHE L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-EDV C 65ICD7568 - FUNCT I N T F REQMTS GN2 L C 3 9 A S / C GSE 05-02-66 LOPG 100-390 KSC-K-DT - L C 3 9 A S / C GSE FUNC I N T F REQ,GOX 02-09-66 LOPG 230-390 KSC-EDV LC-39 02-10-66 L/-FC 230-300 KSC 03-1 9-65 LOPG 100-390 KSC-K-Dl 11-05-54 LO-FC 230-390 IdfC-NAA - PAD B S / C FUNCT I N T F REQS ECS L C 3 9 PAD B S/C-GSE B L C 3 9 L U T GSE SYSTEMS AFRM C O N F I G NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO JRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED - L C 3 9 A ML P I P C R l T + I N T F LOC S / C NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCRD ENTERED NO IRN-CCBD ENTERED F L SYS �I La: APOLLO I N T E R F A C E CONTROL DOCUMENT LOG /I * PAC DATE 2 9 3 U L 66 -. Ld -- --- -- C 3~ D DOCUMENT NUMBER, DOC G S OR R E V I S I O N N O T I C E REV DOCUMENT T I T L E OR CCBD NUMBER --- .................... --........................................ '7 I V' 4 J 651CD7788 - LC39-LUT GSE CABLES-GAS L C 3 9 P H Y I N T F C GOX COND PNL L E A K TS U N I T . . NO IRN-CCBD ENTERED - ACCESS A R M NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD - - -------- -------- ------ --------------- SERV MODULE CABLE REQMTS ENTERED ENTERED ENTERED ENTERED LOFA 239-39C KSC-E 09-22-65 LOFA 270-390 USC-E KSC-E T I M I N G + COUNTDOWN D l S T 09-22-64 LO-FC + CONN 11-29-65 LOFC FUNCT I N T F REQMTS ECS MC LEM S / C G S E 05-03-65 LC 3 4 / 3 7 / 3 9 NO IRN-CCBD NO IRN-CCBD 10-01-64 LC/34/37/39 A-C. - LC34/37/39 - VERT 230-340 230-347 KSC-E LOPG 230-300 KSC-K LOFA 230-340 MSC-F SWG ARM UMB D I S C A 1 4 - 1 7 2 ENTERED' ENTERED ENTERED 230-340 KSC-E CMD MOD ACCESS ARM C A B L I N G 230-340 KSC-D 230-300 HSC-F POWER REC- 8 L C 3 7 / 3 9 LEM NO 1RN-CCBD NO IRN-CCBD NO IRN-CCBD ----a 07-22-65 LEM U M B I L I C A L A N D T E S T CABLES FOR L C 39 NO IRN-CCBD ENTERED A S/C - PREP! INTEGFACE AREAS C E N T E OR C E I NUMBERS A C T l L N I T SYS - + SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA YR MO DA YR CODE SM SWG ARM UMB D I S C A 1 4 0 1 9 ENTERED ENTERED STOP FOR LES* ACCESS ARM * �t APOLLO I N T E R F A C E . CONTROL DOCUMENT LOG DATE 29 J U L 66 P A G E 248 -- --- -- D S _ DOCUMTNT NUMBER* OK R E V I S I O N N O T I C E --- DOC REV DOCUMENT T I T L E OR CCBD NUMBER __--------------------- --------------------------------------NO IRN-CCBD NO IRN-CCBD J 65ICD8304 A MOCK-UP - -------- ------ --------------- ---- I------- ---- ENTERED ENTERED 23 AFRM 9 T O ACCESS ARM WHT RM 03-1 7-65 LOFA KSC-DE C/M ACCESS ARM ADPT HOOD TO S / C I N T F REQ 11-04-65 LOFA MSC-EDV PHY I N T F R E T R A C T I O N MECH Q-BALL ICD-CCBD 5 0 1 - 6 6 - 0 1 6 4 COVER 12-10-65 LO-FA KSC-EDV SATURN V LAUNCH V E H I C L E PROTUBERANCES ICD-CCBD 5 0 1 - 6 5 - 5 2 02-02-66 LOFC MSFC L C 3 9 VAB H I G H BAYS TO L / V 11-19 - 6 5 LOFC KSC-F KSC-EDV-2 ESE/GSE LC 39 VAB LOW BAY AREA TO L / V - E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC - L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC L C - 3 9 PAD AREA L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 0 3 5 12-07-65 LOFC S - I C / M L HOLD DOHN ARMS P H Y S I C A L REQMTS ICD-CCBD 5 0 1 - 6 6 - 0 1 3 6 04-05-66 LO-FC MSFi LOFC MSFC .. LO-EL MSFC-ASTR - - PREPARING I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVTTY - - 65 I C D 9 1 4 2 SCHED ACTUAL R E 1 D A T E R E L DATE PANEL MO DA YR MO D A YR CODE WINO LOAD A L L E V I A T I O N SYS F A C I L TO L / V A F A C I L I T Y C A B L E S FOR LAUNCH V E H I C L E ESE ICD-CCBD 5 0 1 - 6 6 - 0 1 2 3 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 3 09-01-66 03-09-66 �IAO 1 APOLLO I N T E R F A C E CONTROL DOCUMENT LOG 1 DATE 2 9 J U L 66 -- --- -- C H G -- D S , DOCUMENT NUMBER* O R R E V I S I O N NOTICE DOC REV DOCUMENT T I T L E OR CCBO NUMBER --- ....................................... ---i--------------- * R .. A 65ICD9201 R 7 1 NO IRN-CCBD - .- I - A 65ICD9205 -------- -------- ------ --------------- ----- ENTERED LV ESE TO RANGE SEQUENCING 'LC-39 ICD-CCBD 5 0 1 - 6 5 - 8 3 IRN-CCBD 5 0 1 - 6 5 - 8 3 02-11-66 LO-EL 220-370 MS FC-. - L V E S E TO I N S T R SYSTEM ICD-CCBD 5 0 1 - 6 6 - 0 0 8 4 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 6 5 02-11-66 LO-EL 220-290 HS FC- - MSFC COUNT CLOCK T O KSC T I M I N G L C - 3 9 ICD-CCBD 5 0 1 - 6 5 - 8 4 NO IRN-CCBD ENTERED - L V ESE TO KSC DATA MEASUREMENTS 02-11-66 LOEL LOW B A Y ESE TO I N S T R U SYS + REC ICD-CCBD 5 0 1 - 6 6 - 0 1 7 1 02-11-66 LO-EL LOW BAY ESE T O - I N S T R SYS AND REC ICD-CCBD 5 0 1 - 6 6 - 0 0 8 2 02-11-66 LO-EL S E R V I C I N G REQMTS ECS SAT V L C 3 9 ICD-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 IRN-CCBD 5 0 1 - 6 6 - 0 0 3 2 09-09-65 LOPG 250-390 MSFC-K FUNCT I N T F F L U I D REQMTS GHE SYS SAT V 06-28-65 LOPG .-. A 651C09401 PREP4 I N T E R F A C E AREAS CENTS OR C E I NUMBERS ACTIV L V E S E / 6 0 AC POWER REQUIREMENTS ICD-CCBD 5 0 1 - 6 6 - 0 1 7 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 4 ' 65ICD9241 ACTUAL SCHED R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE - �APOLLO INTFRFACE C9NTRDL DOCUMENT LOG AS DATE 29 J U L 6 6 -- --- -- D S - DOCUMENT NUMBER, OR R E V I S I O N NgiTCE DOC REV 510 ----- DOCUMENT T I T L E OR CCBD NUMBER - PREPARING INTERFACE AREAS CENTF" f OR C E I NUMBERS A C T I l -------- -------- ------ --------------- ---------- --- ........................................ - --- SCHEO ACTUAL R E 1 DATE R E L DATE PANEL MO DA Y R M O DA YR CODE -------I------------ NO IRN-CCBD NO IRN-CCBD NO IRN-CCBD PAGE 2 5 0 CONT. ENTERED ENTERED ENTERED F U N C T INTF F L U I D REQMTS GN2 SYS SAT V NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS GH2 SYS SAT V NO IRN-CCBD ENTERED 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS L H 2 SYS SAT V NO IRN-CCBD ENTERED IRN-CCBD 5 0 1 - 6 6 - 0 3 7 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 8 06-28-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS L O X SYS SAT V ICD-CCBD 5 0 1-66-0040 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 0 4 0 06-03-65 LOPG 010-250 KSC-P+VE FUNCT I N T F F L U I D REQMTS RP-1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 1 I RN-CCBD 5 0 1 - 6 6 - 0 0 4 1 06-15-65 COPG 010-250 KSC-" 02-08-66 LO-PG 220-390 MSFC-EDV SYS SAT V FUNCT XNTF F L U I D REQMTS VAB ECS SAT V ICD-CCBD 5 0 1 - 6 6 - 0 0 3 3 NO IRN-CCBD ENTERED -. P I P C R I T APS PROP S E R V I C I N G S A T V ICD-CCBD 5 0 1 - 6 6 - 0 1 5 0 E C' �IAOl A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G PAGE D A T E 29 JUL 66 C H G D DOCUMENTNUMBER, OR R E V I S I O N N O T I C E OOC REV SCHED ACTUAL R E L DATE R E L DATE PANEL no on Y R MO D A YR CODE DOCUMENT T I T L E OR C C B D NUMBER -------- ------- ------ --------------- ------ ....................................... UMB AND SERV CONN P L A T E 3-4 ICD-CCBD 5 0 1 - 6 5 - 4 0 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 9 I R N - C C 8 D 501-66-0289 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 8 08-10-65 S I C AFT UMB + S E R V CONNS P L A T E NO 1-2 I C D - C C B D 501-65-38 I R N - C C B D 501-66-0298 I R N - C C B O 501-66-0286 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 1 S-IC AFT UMB + S E R V CONNS P L A T E NO 3 - 2 I C D - C C B D 501-65-39 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 2 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 2 S-IC AFT , LO-FA 08-1 8 - 6 5 . LO-FA 08-10-65 LO-FA M O T I O N ENV AFT UMB P L A T E S 1q2q+3 S - I C ICD-CCBD 5 0 1 - 6 6 - 0 0 4 2 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 7 08-1 0 - 6 5 LO-FA PHY I C D LAU V E H S - I C ICD-CCBD 5 0 1 - 6 5 - 3 6 IRN-CCBD 50 1-66-0290 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 6 IRN-CCBD 501-66-0378 08-09-65 LO-FA 08-09-65 LO-FA INTK UMB/LC39 PHY I C D L A U V E H S - I C FWD U M B / L C 3 9 ICD-CCBD 5 0 1 - 6 5 - 3 7 I R N - C C B D 501-66-0190 IRM-CCBD 5 0 1-66-0384 NO I R N - C C B D ENTERED , PREPAR I N T E R F 4 f E AREAS C E N T E R OR c E r NUMBERS ACTIVI GSE GSE o i o - 2 10 KSC-P+' �APOLLO I N T Z R F A C E CONTROL. DQCUMENT L D G IAOl P A G E 252 D A T t 2 Y J U L -46 -- D S --- -- DOCUMENT NU' OR R E V I S I O N --- _ DOC REV DOCUMENT T I T L E OR CCBD NUMBER --- ........................................ "3 - UMB + SERV CONNECTIONS S - I I ICD-CCBD 501-66-0111 IRN-CCBD 5 0 1 - 6 6 - 0 1 1 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 8 3 - - SCHED ac~ukt R E L DATE R E L D A T E P A N E L MO DA YR MO D A YR CODE PREPAP,ING I N T E R F A C E AREAS CENT: OR C E I NUMBERS ACTIVITY -------- -------- ------ -------------- ---------06-28-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S I X L O X DISCONNECT ICD-CCBD 5 0 1 - 6 6 - 0 1 2 7 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 7 06-21-65 LO-FA 020-390 KSC-P+VE U M B I L I C A L + SERV CONN S - 1 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 6 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 6 06-21-65 LO-FA 020-390 KSC-P+VE 06-28-65 LO-FA ,020-390 KSC-P+VE 06-21-65 LO-FA 040-390 KSC-P 06-18-65 LO-FA 040-390 KSC-PIVF 06-1 8 - 6 5 LO-FA 090-390 KSC-P+Vf XNTERM LH2 D I S C U M B I L I C A L + S E R V I C E CONN S - I 1 ICD-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 5 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 7 NO IRN-CCBD ENTERED FORWARD - UMB + SERV CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 8 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 8 - UMB + S E R V I C E CONNECTIONS S - I V B ICD-CCBD 5 0 1 - 6 6 - 0 1 7 7 IRN-CCBD 5 0 1 - 6 6 - 0 2 8 3 - U M B I L I C A L + S E R V I C E CONNECTIONS I U ICD-CCBD 5 0 1 - 6 5 - 3 5 AFT FORWARD . "E �,) APOLLO I N T E R F A C E CONTROL DOCUMENT LOG ) PAGE .DATE 2.9 JUL 66 -- --- -- C H G \--/ IAOl DOCUMENT NUMBER, 9 R R E V I S I O N NOTICE DOC REV -S -------------------- --- SCHED ACTUAL R E 1 D A T E R E L DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER PREPAR I N T E R F A C E AREAS CENTER OR C E I NUMBERS ACTIVI -------- -------- ------ -------------- ------ -----------------------------,----- IRN-CCBD 5 0 1 - 6 6 - 0 2 8 5 IRN-CsCBD 50 1 - 6 6 - 0 2 8 4 J 651CD9753 \ . . - PHY TCD S - I VB PNEU CONS D S V - 4 8 - 4 3 2 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 7 V 06-21-65 LO-FA 220-390 K S C-K- PHY I C D S - I V B PNEU CONS O S V - 4 8 - 4 3 3 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 5 V 06-21-65 LO-FA 220--390 USC-P+ PNEU CONS SET L C 3 9 01-28-66 LO-FA 010-390 KSC-P+ 06-21-65 LO-FA 220-390 KSC-P+ 09-15-65 LO-FA 220-390 MSFC-E 09-15-65 LO-FA 220-390 MSFC-E 06-21-65 LO-FA 220-390 .KSC-P+ P I P I N G CRITERIA S-IVB ICD-CCBD 5 0 1 - 6 6 - 0 0 4 3 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 4 - PHY I C D S - I VB H T EXCH D S V - 4 8 - 4 3 8 / S A T ICD-CCBD 5 0 1 - 6 6 - 0 1 0 6 - PHY I C D I U C O O L I N G U N I T + P I P I N G C R I T ICD-CCBD 5 0 1 - 6 5 - 4 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 7 6 - - PHY I C D ICD-CCBD IRN-CCBD V I U PNEU CONS + P I P I N G C R I T E R I A 501-65-48 501-66-0292 PHY I C D APS PNEU CONS 'DSV-4B-436/SAT . . . ICD-CCBD 5 0 1 - 6 6 - 0 ' 1 0 4 V - P I P I N G C R I T E R I A APS PNEU CONSOLE L C 3 9 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 4 02-10-66 LOFA 220-390 HSFC-E PHY I C D S - I C I N E R T . P R E F I L L + P I P I N G C R I Y , . ICD-CCBD 5 0 1 - 6 5 - 4 7 09-15-65 LO-FA 220-390 MSFC-E �APOLLO I N T E R F A C E CONTROL DOCUMENT L O G DATE 2 9 J U L 66 -- DOCUMENTNUMBERI OK R E V I S I O N N O T I C E D S _ PAGE 2 5 4 --- -- --- DOC REV SCHED ACTUAL R E L D A T E R E 1 DATE PANEL MO DA YR MO DA YR CODE DOCUMENT T I T L E OR CCBD NUMBER -------- -------- ------ ------------- --- ........................................ ----------------I--- - - 65 I C D 9 7 6 6 - 0 0 3 PHY I C D S - I I PNEU CONSOLES S 7 - 4 1 B / S A T ICD-CCBD 5 0 1 - 6 5 - 2 8 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 4 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 1 PHY I C D S I I PNEU CONSOLE S 7 - 4 1 C / S A T ICD-CCBD 501-65-29 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 8 I RN-CCBD 5 0 1 - 6 6 - 0 2 9 4 PHY I C D S I I PNEU CONS S 7 - 4 1 A + 4 1 D / S A T ICD-CCBD 5 0 1 - 6 5 - 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 0 IRN-CCBD 5 0 1 - 6 6 - 0 3 0 0 PHY I C D HEAT EXCHANGER A 7 - 7 1 / S A T ICD-CCBD 5 0 1 - 6 5 - 3 1 IRN-CCBD 5 0 1 - 6 6 - 0 2 9 5 IRN-CCBD 5 0 1 - 6 6 - 0 1 3 1 PIPING CRITERIA S-I1 ICD-CCBD 5 0 1 - 6 6 - 0 0 4 5 IRN-CCBD 5 0 1 - 6 6 - 0 3 2 7 .CD9769 V V V V PNEU SYS/SATURN V --------- 06-2 5-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 06-25-65 LO-FA 220-390 KSC-P+VE 220-390 MSFC-EDV / 02-1 1-66 LO-FA * SEE B A S I C NUMBER FOR R E V I S I O N ~ T I T L E I E T C ~ - PHYS I C D S - I C H Y D R A U L I C U N I T L C 3 9 ICD-CCRD 5 0 1 - 6 6 - 0 1 8 3 0 2 - 1 0-66 LO-FA 220-390 KSC-K-DT - PHY I C D S - I C PNEU CONSOLE RKS 1 - 2 - 3 + 4 09-1 5 - 6 5 ' LO-FA 220-390 K S C-K-CT 08-09-65 LO-FA ICD-CCBD ; G PREPARING I N T E R F A C E AREAS CENTEP OR C E I NUMBERS ACTIl ! - SEE-DUG 50 1-65-61 PHY i C D FNEU C Q N S S i E S 5 1 6 . 7 + 8 S-IC - �A P O L L O I N T E R F A C E CONTROL DOCUMENT L O G 2 D A T E 29 J U L 66 DOCUMENT N U M B E R * OR R E V I S I O N N O T I C E .................... DOC REV DOCUMENT T I T L E OR C C B D NUMBER --- ...................................... ICD-CCBD - - 9 - PREP& I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIb -------- -------- ------ --------------- ----- 501-65-34 PHY I C D S - I C PNEU CHECKOUT RKS 1-2-3+4 ICD-CCBD 5 0 1 - 6 5 - 4 6 09-24-65 LO-FA 220-390 MSFC- PIPING CRITERIA S-IC I C D - C C B D 5 0 1-66-0046 IRN-CCBD 5 0 1-66-0306 02-07-66 LO-FA 220-280 HSFC- 12-09-65 LO-FA 210-390 KSC-E P I P C R I T S - I C F L U S H + PURGE U N I T S A T V ICD-CCBD 5 0 1 - 6 6 - 0 0 4 7 02-07-66 LO-FA 010-390 HSFC- PHY I C D + P I P E C R I T S T 1 L E A K DETECT SYS ICD-CCBD 5 0 1 - 6 6 - 0 1 5 5 I R N - C C B D 501-66-0264 IRM-CCBD 5 0 1 - 6 6 - 0 2 7 4 02-10-65 LO-FA 020-220 HSFC- P H Y I C D P I P E C R I T S I C FWD UMB S E R V U N SV I C D - C C O D 501-66-0180 02-10-66 LO-FA 010-220 MSFC- PNEU CONSOLE S E T A S - I 1 S T A G E GSE PLACEMENT ON M B L LAUNCHER ICD-CCBD 5 0 1 - 6 6 - 0 1 2 9 IRN-CCBD 5 0 1 - 6 6 - 0 1 2 9 - SCHED ACTUAL REL DATE R E L DATE PANEL MO D A YR MO D A YR CODE SEE-DWG SEE B A S I C NUMBER F O R R E V I S I O N t T I T L E t E T C PHY I C D + P I P C R I T H A Z GAS A N A L Y Z E R S A T V ICD-CCBD 5 0 1 - 6 6 - 0 1 0 0 IRM-CCBD 50 1-66-0377 IRN-CCBD 5 0 1 - 6 6 - 0 3 1 5 02-04-66 LO-FA PHY LOC PORT I U WATER ACCUM CART 03-02-66 LO-FA . A L C 3 9 ML 220-000 .. HSFC- �APO.LL0 I Y T E R F A C E CONTROL OOCUMENT L O G DATE 29 J U L 66 AS -- --- -- G S - DOCUMENT NUMBER* OR R E V I S I O N N U T I C E ----------------.---- 66ICD7007 66 I C D 7 0 0 9 A 80M90SlO DOC REV 510 ----- DOCUMENT T I T L E OR CCBD NUMBER CONT. --- -----------_--------------------------- - L C 3 9 S / C D-C. - F L I G H T MECHANICS PANEL I C D LC-39 PAGE 256 --- SCHED ACTUAL R E L D A T E R E L DATE PANEL MO DA YR MO DA YR CODE PREPb?ING I N T E R F A C E AREAS CEN'i OR C E I NUMBERS ACTIVITY -------- -------- ------ --------------- ---------02-08-66 LOFC 230-390 KSC 01-20-66 LOFC 230-390 KSC-EDV-2 09-09-99 FM 000-100 HSFC-AERO H A Z A R D P R O O F ~NG-SIC POWER S U P P L I E S IA31 ' �IA 0 1 A P O L L O I N T E R F A C E C O N T R O L DOCUMENT L O G -\ PAG -- --- -- DATE 2 9 J U L 66 -I ?c C' -, I$ 3 -A -\ H 1 G L D O C U M E N T NUMBER, OR R E V I S I O N N O T I C E DOC REV - +++ A SON36801 E 65ICD9041 I E 65ICD9080 - DOCUMENT T I T L E OR C C B D NUMBER I C D SATURN I B / V SCHED ACTUAL REL DATE REL DATE PANEL MO D A Y R MO D A YR CODE PREPA I N T E R F A C E AREAS CENTE OR C E I NUMBERS ACTIV C O N T R O L R A T E GYRO P K G LC 3 9 V A B LOW B A Y A R E A ' T O ' L / V - E S E / G S E I C D - C C B D 501-66-0086 02-09-66 LO-FC 720-390 KSC-El LC39 MSS T O L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-El �IAOl APOLLO I N T E R F A C E CDYTRfli. DOCUMENT LOG PAGE 2 5 8 DATE 2 9 J U L 66 --- -- --- -- D S DOCUMENT NUMBER, OR R E V I S I O N N C I I C E DOC REV DOCUMENT T I T L E OR CCBD NUMBER - -------------------- --- ---------------------------------------A 50M36801 E 65ICD9041 - - I C D SATURN I B / V CONTROL RATE GYRO P K G SCHED ACTUAL R E L DATE R E L DATE PANEL MO DA Y R MO DA YR CODE PREPCI" I N G I N T E R F A C E AREAS CENT OR C E I N U M B E R S ACTIVITY -------- ------- ------ --------------- ---------03-1 5-66 M- NF LC 3 9 VAB LOW B A Y AREA TO L / V - E S E / G S E 1CD-CCBD 5 0 1 - 6 6 - 0 0 8 6 02-09-66 LO-FC L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 040-090 MSFC-M-ED �APOLLO I N T E R F A C E CONTROL DOCUMENT LOG ' D A T E 2 9 J U L 66 -- --- -- , -4 -1' . SCHED D S DOCUMENT NUMBER, OR R E V I S I O N N O T I C E DOC REV - - - DOCUMENT T I T L E OR CCBD NUMBER I C D SATURN I B / V ACTUAL R E L DATE R E L DATE PANEL HO D A YR MO DA YR CODE PREP I N T E R F 4 C E A R E A S CENT OR C E I NUMBERS ACT1 CONTROL RATE GYRO PKG LC 3 9 V A 8 LOW B A Y AREA TO. L / V - E S E / G S E ICD-CCBD 50 1 - 6 6 - 0 0 8 6 L C 3 9 MSS TO L / V ESE/GSE ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 02-14-66 LO-FC 220-390 KSC-I: �APOLLO I N T E R F A C E CONTRni - O 5 - .DATE 29 J U L 66 AS -- -.-- -- DOCUMENT NUMBER, 3R R E V ! S I O N N C T I C E ----------------.-I-- DOC REV - 514 DOCUMENT T I T L E OR C C B D NUMBER t 65ICD9041 - I C D SATURN . I B / V 1 A31 PAGE 260 --- ----- --- ........................................ 4 50M3bdOL DOCUMENT L O G SCHED ACTUAL R E L D A T E REL D A T E PANEL MO D A YR MO D A YR CODE PREr 4G -------- -------- ------ --------------- ---------INTERFACE A R E A S C E N T E R OR C E I NUMBERS ACTIVITY CONTROL R A T E GYRO P K G L C 3 9 V A B LOW B A Y AREA T O L / V - E S E / G S E I C D - C C B D 501-66-0086 02-09-66 LO-FC 220-390 KSC-EDV-2 L C 3 9 MSS TO L / V E S E / G S E I C D - C C B D 501-66-0110 02-14-66 LO-FC 220-390 KSC-EDV-2 �A P U L L O INTERFAf;E DATE 2 9 Jut CONTROL UOCUMENT LOG PAC; 66 -- --- -- O ,-. DOCUMENT NUMBER, n q REVISION NOTICE DOC REV DOCUMENT TITLE OR C C B D NUMBER ____-__-----_-_-- ........................................ - LC. 3 9 V A B LOU 8 A Y AREA ICD-CCBD 5 0 1 - 6 6 - 0 0 8 6 L C 3 9 MSS TO L / V E S E / G S E ICD-CCBD 5 0 1 - 6 6 - 0 1 1 0 T O L/-V-ESE/GSE' SCHED ACTUAL REL D A T E R E L DATE P A N E L MO DA YR MO DA YR CODE -------- -------- ------ PHEPAl I N T E R F A C E AREAS CENTEI OR C E I NUMBERS ACTIV ------ -----I-------- 02-09-66 LO-FC 220 - 3 9 0 KSC-EL 02-14-66 LO-FC 220-390 KSC-EI. � Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000069 Title A name given to the resource Reproduction of "Apollo Interface Control Document Log." Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. X66-94268 Description An account of the resource This copy is a reproduction of a document held by the NASA Scientific and Technical Information Facility . Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1966-07-29 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn Project (U.S.) Project Apollo (U.S.) Information management Type The nature or genre of the resource Logs (records) Text Source A related resource from which the described resource is derived Saturn V Collection University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000051_000074 https://digitalprojects.uah.edu/files/original/20/1284/spc_stnv_000142.pdf 77fbfe010026bb6e2d609c82c4d4a9a7 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000142 Title A name given to the resource "A Bibliography of Wernher von Braun, 1967." Description An account of the resource This official bibliography includes English- and foreign-language books, articles, and interviews. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1968-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Von Braun, Wernher, 1912-1977 Communication in science German Americans Saturn Project (U.S.) Type The nature or genre of the resource Bibliographies Text Source A related resource from which the described resource is derived Saturn V Collection Box 25, Folder 7 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000119_000149 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17815 https://digitalprojects.uah.edu/files/original/20/1285/spc_stnv_000143.pdf ac8a57554dbbaca865efb65710a5c5fc Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000143 Title A name given to the resource "Aero-Astrodynamics Laboratory Bimonthly Progress Report, April and May 1967." Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Aero-Astrodynamics Laboratory Date A point or period of time associated with an event in the lifecycle of the resource 1967-06-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource NASA space programs Project management Saturn Project (U.S.) Type The nature or genre of the resource Progress reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 22, Folder 30 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000119_000149 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17690 https://digitalprojects.uah.edu/files/original/20/1287/spc_stnv_000146.pdf ab252a1a5e031df7b165e4ebc1ebd047 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000146 Title A name given to the resource "Aero-Astrodynamics Laboratory Bimonthly Progress Report, December 1967-January 1968." Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Aero-Astrodynamics Laboratory Date A point or period of time associated with an event in the lifecycle of the resource 1968-02-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource NASA space programs Project management Saturn Project (U.S.) Type The nature or genre of the resource Progress reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 25, Folder 23 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000119_000149 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17831 https://digitalprojects.uah.edu/files/original/20/1623/Binder1_062508100607.pdf 95595aae748475018cceeb7cd1c2bc86 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Title A name given to the resource Saturn V Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/60" target="_blank" rel="noreferrer noopener">View the Saturn V Collection finding aid in ArchivesSpace</a> Identifier An unambiguous reference to the resource within a given context Saturn V Collection Description An account of the resource <p>The Saturn V was a three-stage launch vehicle and the rocket that put man on the moon. (Detailed information about the Saturn V's three stages may be found<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_first_stage.html">here,<span> </span></a><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_second_stage.html">here,<span> </span></a>and<span> </span><a href="https://www.nasa.gov/centers/johnson/rocketpark/saturn_v_third_stage.html">here.</a>) Wernher von Braun led the Saturn V team, serving as chief architect for the rocket.</p> <p>Perhaps the Saturn V’s greatest claim to fame is the Apollo Program, specifically Apollo 11. Several manned and unmanned missions that tested the rocket preceded the Apollo 11 launch. Apollo 11 was the United States’ ultimate victory in the space race with the Soviet Union; the spacecraft successfully landed on the moon, and its crew members were the first men in history to set foot on Earth’s rocky satellite.</p> <p>A Saturn V rocket also put Skylab into orbit in 1973. A total of 15 Saturn Vs were built, but only 13 of those were used.</p> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_stnv_000150 Title A name given to the resource Publication listing. Description An account of the resource The document is a list of tools from the Manufacturing Engineering Laboratory at MSFC. Included in the list are the tool numbers, titles, and stages of development. Prior to the list the document includes a handwritten note from Bill Vardaman. Issue April 1968. Office R-ME-TDP. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1968-03-27 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Project Apollo (U.S.) Saturn Project (U.S.) George C. Marshall Space Flight Center. Manufacturing Engineering Laboratory. Source A related resource from which the described resource is derived Saturn V Collection Box 26, Folder 9 University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_stnv_000150_000174 https://digitalprojects.uah.edu/files/original/87/1948/spc_conr_000054_000063.pdf 9b45b592e273dea31abb99212e95939e Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Gertrude Conard Collection Title A name given to the resource Gertrude Conard Collection Description An account of the resource Gertrude Conard (February 17, 1924 to May 20, 2008) was the personal secretary of William R. Lucas, the fourth Director of the George C. Marshall Space Flight Center (MSFC). Conard worked for NASA for 39 years. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/16">View the Gertrude Conard Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_cona_000054_000063 Title A name given to the resource Program from "Life in the Universe," the Sixth Annual Von Braun Exploration Forum. Date A point or period of time associated with an event in the lifecycle of the resource 1993-09-21 Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Description An account of the resource The program includes biographic sketches of the Forum speakers, as well as songs performed by guest speaker and space enthusiast John Denver. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Temporal Coverage Temporal characteristics of the resource. 1990-1999 Subject The topic of the resource Denver, John Tarter, Jill C. Uhl, Edward George Chappell, Rick, 1943- Henry, Joe Von Braun, Wernher, 1912-1977 Huntsville (Ala.) Type The nature or genre of the resource Programs Still Image Text Source A related resource from which the described resource is derived University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/87/1949/spc_conr_000064_000073.pdf bfe73985f5ae354f6b6f9ee21ad9e88a Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context Gertrude Conard Collection Title A name given to the resource Gertrude Conard Collection Description An account of the resource Gertrude Conard (February 17, 1924 to May 20, 2008) was the personal secretary of William R. Lucas, the fourth Director of the George C. Marshall Space Flight Center (MSFC). Conard worked for NASA for 39 years. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/16">View the Gertrude Conard Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_cona_000064_000073 Title A name given to the resource Program from "He Conquered Space," the Ninth Annual Von Braun Exploration Forum. Date A point or period of time associated with an event in the lifecycle of the resource 1996-10-18 Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Description An account of the resource The program includes biographical sketches of the speakers, including John S. Hendricks, Rick Chappell, and Walter Cronkite. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Temporal Coverage Temporal characteristics of the resource. 1990-1999 Subject The topic of the resource Cronkite, Walter Chappell, Rick, 1943- Hendricks, John S., 1952- Von Braun, Wernher, 1912-1977 Type The nature or genre of the resource Programs Still Image Text Source A related resource from which the described resource is derived University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/195/3336/spaceintelligencenotes_19601101.pdf efe50f62666dc0c9743931b69691c1f4 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19601101 Title A name given to the resource <i>Space Intelligence Notes</i>, November 1, 1960. Description An account of the resource This is Vol. 1, No. 1 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include the use of television in Soviet space research to transmit pictures of the reverse side of the Moon to Earth, a proposed plan to use a ring of small particles around the Earth to create heat and light, an experimental Soviet space ship in orbit with two dogs onboard and other essentials for future manned flights, a Soviet published book on problems associated with flights to the Moon, discoveries and theories of the composition of the surface of the Moon, and international reactions to U-2 flights over Russia. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1960-11-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Outer space--Exploration Satellites--orbits Serial publications Space flight Space race United States--Relations--Soviet Union Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3337/spaceintelligencenotes_19601201.pdf 669bc75241897f491fa3967115aa3570 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19601201 Title A name given to the resource <i>Space Intelligence Notes</i>, December 1, 1960 Description An account of the resource This is Vol. 1, No. 2 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include part one of an in-depth look at Russian literature and technology in the field of astronautics, various topics of Soviet space-related activities, and articles pertaining to the future of the industry. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1960-12-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3338/spaceintelligencenotes_19610101.pdf 4f8de1d164e8d36c319276c6f076d3b1 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610101 Title A name given to the resource <i>Space Intelligence Notes</i>, January 1, 1961. Description An account of the resource This is Vol. 2, No. 1 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include available Soviet scientific literature including scientific journals available in English, part two of an in-depth look at Russian literature and technology in the field of astronautics and various topics of Soviet space-related activities. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-01-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3339/spaceintelligencenotes_19610201.pdf a123794a08f6356ce172241d9163f163 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610201 Title A name given to the resource <i>Space Intelligence Notes</i>, February 1, 1961. Description An account of the resource This is Vol. 2, No. 2 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include the Soviet's goal of converting its industrial production to automation, the next Russian space "spectacular", Hungarian space goals, problems of interplanetary travel, the significance of spaceships in the study of the atmosphere, and Intelligence Briefs. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-02-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3340/spaceintelligencenotes_19610301.pdf 7a8a5420abffd719e5f345f39d4d6f67 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610301 Title A name given to the resource <i>Space Intelligence Notes</i>, March 1, 1961. Description An account of the resource This is Vol. 2, No. 3 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include the "rise of the Soviet intelligentsia", Soviet publications regarding future developments in astronautics, a contract signed between the Soviets and a New York publisher for exclusive English language rights to Soviet scientific books, the development of cosmic microbiology, a review of the danger of radiation sickness, and Intelligence Briefs. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-03-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3341/spaceintelligencenotes_19610400.pdf 3258d355a9ffb81746db82f45dd20813 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610400 Title A name given to the resource <i>Space Intelligence Notes</i>, April 1961. Description An account of the resource This is Vol. 2, No. 4 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include featured articles of "The Hidden Side of the Moon" and "The Soviet Venus Probe," Soviet rockets study the eclipse, and Intelligence Briefs. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-04 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Space flight Space race United States--Relations--Soviet Union Huntsville (Ala.) Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3342/spaceintelligencenotes_19610500.pdf 3ccf402e4c42a3f9fe0282dc2deeb2a1 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610500 Title A name given to the resource <i>Space Intelligence Notes</i>, April 1961. Description An account of the resource This is Vol. 2, No. 5 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include featured articles of "Soviet Security" and "Soviet Space Feat Confirmed," Soviet testing of glass fiber nuclear fuel, Soviet space medicine, flying saucers in Russia, the failure to re-establish radio contact with the Venus probe, data on the Tungusska meteorite, and details of the first Soviet manned satellite orbit. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-05 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Outer space--Exploration Satellites--orbits Serial publications Space flight Space race United States--Relations--Soviet Union Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3343/spaceintelligencenotes_19610600.pdf b47fd3e0219bc838ec0315081e041348 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610600 Title A name given to the resource <i>Space Intelligence Notes</i>, June 1961. Description An account of the resource This is Vol. 2, No. 6 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include various featured articles about Soviet meteorological satellites, rocket planes and cosmoplanes, Youri Gagarin on the manned Soviet space flight, various planets, telescopes and instruments, lunar catalog, human colonization of planets, space physics and geophysics, animal experiments during space flights, space stations, Soviet space carrier vehiclce launching technique, literature on devices used in USSR satellites, women and laboratories in space, Soviet literature, and available technician information. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-06 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3344/spaceintelligencenotes_19610700.pdf f0b1227cdfb9938e051d87cceeb8c617 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610700 Title A name given to the resource <i>Space Intelligence Notes</i>, July 1961. Description An account of the resource This is Vol. 2, No. 7 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include a comparison of Soviet and American satellites, the thermal history of the moon, the Earth's third radiation belt, observations of Venus and the view that Venus does not rotate, natural Earth satellites, signal from space unidentifiable, Soviet proposal of new lunar TV satellite, and the possibility of Soviet women in space. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-07 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3345/spaceintelligencenotes_19610800.pdf ecb19986fd0b1c85e0c008fd8625c661 Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610800 Title A name given to the resource <i>Space Intelligence Notes</i>, August 1961. Description An account of the resource This is Vol. 2, No. 8 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include problems in the Soviet scientific community due to the shift of power and other changes, espionage and outer space, Soviet fishermen observe the return of two American astronauts from space, plenary session of the Commission of Radioastronomy, Soviet discussion of the Venus shot, and radar observations of Venus. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-08 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3346/spaceintelligencenotes_19610900.pdf e272778a7e4745cce44415f96864af3a Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_19610900 Title A name given to the resource <i>Space Intelligence Notes</i>, September 1961. Description An account of the resource This is Vol. 2, No. 9 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include NASA translations of Soviet publications, the satellite orbit of Vostok 2, the space launching of Soviet spacecraft, a reported luminescent ionosphere around Venus, Russian plans for a manned space station, possible Russian concentration on rocket shots at the Moon, new volumes available of a Soviet space publication on artificial Earth satellites, transmission into space with AM short-wave telegraph-telephone transmitters, Soviet high-speed photoelectric spectrophotometer, future Soviet space communication techniques, and various Soviet experiments, research, and discoveries. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-09 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02 https://digitalprojects.uah.edu/files/original/195/3347/spaceintelligencenotes_19611000.pdf babe979cb2f111c567228460470f2aad Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context <em>Space Intelligence Notes</em> Title A name given to the resource <em>Space Intelligence Notes</em> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spaceintelligencenotes_1961100 Title A name given to the resource <i>Space Intelligence Notes</i>, October 1961. Description An account of the resource This is Vol. 2, No. 10 of Space Intelligence Notes, a publication of the Space Systems Information Branch at the Marshall Space Flight Center. Topics include the second list of NASA translations of Soviet publications, a detailed account and analysis of the flight of the Soviet satellite Vostok II, the revealing of the international satellite communications system SPACEWARN, Russian study of anabiosis for possible use in space flight, the retardation of Earth's rotation, the development of an experimental model of an electromagnetic flowmeter by the Russians and their success in converting glass into microcrystalline materials, and various other studies conducted by the Soviets. Creator An entity primarily responsible for making the resource George C. Marshall Space Flight Center Date A point or period of time associated with an event in the lifecycle of the resource 1961-10 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Astronautics--Soviet Union--History Outer space--Exploration Satellites--orbits Serial publications Soviet literature Space flight Space race United States--Relations--Soviet Union Type The nature or genre of the resource Newsletters Text Source A related resource from which the described resource is derived Serials University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama Language A language of the resource en Rights Information about rights held in and over the resource This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. Relation A related resource spc_intelligence_notes_2021_02