272 20 8242 https://digitalprojects.uah.edu/files/original/20/10615/relipreddesideci_062107154123.pdf 684eb3d1283c479e5eaaf7324fa17a6b 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 relipreddesideci_062107154123.pdf spc_stnv_000652 Title A name given to the resource "Purchasing and contracting at the George C. Marshall Space Flight Center." Description An account of the resource This is a speech given to fellow purchasing agent regarding purchasing and contracting. Creator An entity primarily responsible for making the resource Wood, A. J. Date A point or period of time associated with an event in the lifecycle of the resource 1964-01-20 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Contract management Project management Type The nature or genre of the resource Text Speeches Source A related resource from which the described resource is derived Saturn V Collection Box 10, 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_000650_000674 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/16902 https://digitalprojects.uah.edu/files/original/20/1156/spc_stnv_000072.pdf 2ec7547066c97c2fd55fea4efa5420fd PDF Text Text ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............. .......................... ............ ............. ............ ............... . N A T I O N A L A E R O N A U T I C S A N D SPACE ADMINISTRATIO ............................. .......... .:..,. . . .,&:.:.:.:.:.:.:.:.: . i.x:.:.:.:.:.:.:.:.:. ..................... ............ ............. FINAL ;;,. ..,........... ............. ..., .... .;. ..&:::::::: ...................... . . . . . . . . .SATURN I-IISTORY CCCUMENT .......... ................... . . ............. . .............. . . . . . . . ...... Universi~yof: Alabcma Ec :.-arch !nstitute 1 - a .:- !<j.%.:.:.:.:.:.:.:.:. History of Science C. Tecl..nofcgy Group .., . ?.-.~.-.~.~.~.~.~.~.~.~ . ,;-:*.:.:.:.:.;.;.:.:.:.:.:. ..... .i' ............... * ........... Date --- - - - - - - - Doc. No. - - - ----........... ............ ............. ............. ... ....,,. . .!<' ........... ..... ...*....-.m...-.*.*,-.-...-.-. c.;: .. .*;:+:.::.>>:.:.:.:. +:.-......: ............. .:?........::... . ............................. ............ .................. ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ PREPARED BY ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ LUNAR SURFACE OPERATIONS 0 FFICE ........... ............ ........... ............ ........... ............ ........... MISSION OPERATI.0NS BRANCH ............ ........... ............ ........... ............ ........... ............ ........... FLIGHT CREW SUPPORT DIVISION ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ JUNE 27,1969 ........... ............ ........... ............ ........... < ., : . , 11;';. , ,: a : , , . ', '. x .$., ~ *.~,:t.: ; . I + ,,,,---,, APOLLO 11 LUNAR SURFACE OPERATIONS PLAN M A N N E D SPACECRAFT C E N 1 HOUSTON.TEXAS ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... ............ ........... �FINAL EDITION APOLLO I1 LUNAR SURFACE OPERATIONS PLAN JUNE 13, 1969 Prepared by : w.. H . Wood, Jr. Lunar Surface operatio$. Off i c e Approved by : Lunar surflace Operations Off i c e H . A. Kuehnel Chief, Mission Operations Branch - C. H . Woodling \ \ Assistant Chief f o r Crew'Tra3,ning Chief, fight brew Support Division S~c33 k -. U ... . - Donald K . Slayton /\ Director of Flight( c ew Operations - -3 �APOLLO 11 LUNAR SURFACE OPERATIONS PLAN (FINAL EDITION) PREFACE This document h a s been prepared by t h e F l i g h t Crew Support D i v i s i o n , F l i g h t Crew Operations D i r e c t o r a t e , Manned S p a c e c r a f t C e n t e r , Houston, Texas. The i n f o r m a t i o n contained w i t h i n t h i s document r e p r e s e n t s t h e Lunar S u r f a c e Operations P l a n f o r Ap0110'11, t h e f i r s t planned l u n a r landing m i s s ion. T h i s i s t h e f i n a l e d i t i o n of t h e Apollo 11 Lunar S u r f a c e Operations P l a n . The p l a n i s under t h e c o n f i g u r a t i o n c o n t r o l of t h e Crew Procedures Control Board (CPCB) and a l l proposed changes t o t h i s document should b e submitted t o t h e CPCB v i a a Crew Procedures Change Request. Changes and comments t o t h e p l a n should b e d i r e c t e d t o W. H. Wood, Jr., Lunar S u r f a c e Operations O f f i c e , FCSD. �CONTENTS Page Preface iii L i s t of F i g u r e s and Tables vii 1.0 INTRODUCTION 1 2.0 MISSION PLAN 2.1 2.2 2.3 3.0 Mission Mission Summary 2.3.1 2.3.2 Purpose Description of Mission Requirements Introduction Mission Objectives and Experiments NOMINAL LUNAR EVA 3.1 3.2 3.3 3.4 3.5 Timeline D e s c r i p t i o n and R a t i o n a l e 3.1.1 Lunar Surface Stay 3.1.2 Extravehicular Activity Task and Data D e s c r i p t i o n s 3.2.1 Environmental F a m i l i a r i z a t i o n 3.2.2 Preliminary Checks 3.2.3 T e l e v i s i o n Coverage 3.2.4 S-band E r e c t a b l e Antenna Deployment 3.2.5 Photography 3.2.6 EVA and Environment E v a l u a t i o n 3.2.7 Sample C o l l e c t i o n s 3.2.8 LM I n s p e c t i o n 3.2.9 Experiment Deployments 3.2.10 Use of Lunar Equipment Conveyor 3.2.11 EVA Termination Summary Timeline Timeline D e t a i l e d Procedures 3.5.1 Nominal A c t i v i t i e s Sequence 3.5.2 Procedures �ALTERNATE AND CONTINGENT PLANS 4.1 4.2 4.3 A l t e r n a t e EVA (With S-band E r e c t a b l e Antenna ~ e p l o y m e n t ) 4.1.1 D e s c r i p t i o n and R a t i o n a l e 4.1.2 Summary T i m e l i n e 4.1.3 Timeline 4.1.4 D e t a i l e d Procedures C o n t i n g e n t EVA 1-Minimum Time, One Man 4.2.1 D e s c r i p t i o n and R a t i o n a l e 4.2.2 Summary T i m e l i n e 4.2.3 Timeline C o n t i n g e n t EVA 2-One Man, Two Hours 4.3.1 D e s c r i p t i o n and R a t i o n a l e 4.3.2 Summary T i m e l i n e 4.3.3 Timeline APPENDIX 5.1 5.2 5.3 5.4 5.5 Abbreviations D e t a i l e d O b j e c t i v e s and Experiments 5.2.1 Introduction 5.2.2 Definitions 5.2.3' Objectives 5.2.4 Experiments Lunar S u r f a c e O p e r a t i o n a l C o n s t r a i n t s 5.3.1 Introduction 5.3.2 Constraints Classification 5.3.2.1 Constraint Categories 5.3.2.2 Violation Classification 5.3.3 Mission O p e r a t i o n s C o n s t r a i n t s 5.3.4 Lunar S u r f a c e O p e r a t i o n s C o n s t r a i n t s 5.3.5 Equipment O p e r a t i o n C o n s t r a i n t s 5.3.6. Equipment Design C o n s t r a i n t s 5.3.7 General C o n s t r a i n t s Nominal Lunar S u r f a c e EVA M e t a b o l i c P r o f i l e s 5.4.1 Introduction 5.4.2 CDR M e t a b o l i c P r o f i l e 5.4.3 LMP M e t a b o l i c P r o f i l e References PAGE �FIGURES Figure Number Title Lunar s u r f a c e a c t i v i t y t i m e l i n e f o r 22-hour s t a y Radar coverage during l u n a r . s t a y f o r launch d a t e of J u l y 16 . TV f i e l d of view from MESA TV f i e l d of view from t r i p o d (with Lunar Day lens) Quad I i n s p e c t i o n p o i n t s Quad I1 i n s p e c t i o n p o i n t s Quad 111 i n s p e c t i o n p o i n t s Quad I V i n s p e c t i o n p o i n t s Probable a r e a s f o r l u n a r s u r f a c e a c t i v i t y TABLES Table No. 3- 1 Performance margins f o r LM communications 3-2 Loose equipment l e f t on l u n a r s u r f a c e vii Page , 12 �SECTION 1.0 INTRODUCTION �1.0 INTRODUCTION This final edition of the Lunar Surface Operations'Plan defines equipment requirements, crewlequipment interfaces, and final flight planning and crew activities for lunar surface EVA operations during the first manned lunar landing mission. This plan delineates how the lunar surface operational and scientific objectives for the first manned lunar landing mission will be accomplished through pre-mission timelining and procedures definition. Although the primary concern of this plan is the lunar surface EVA operational aspects of the mission, interface relationships are presented to provide clarity and continuity to the overall mission plan. The nominal plan is for a single two-man lunar excursion. The planned duration will be two hours and forty minutes or upon reaching a pre-determined red line on one of the PLSS consumable~. The red line is defined as having either a 30 minute supply of oxygen or a 30 minute supply of feedwater remaining after repressurization. The battery is not considered to be a constraint on the lunar surface time for this mission. Based on an estimation of each crewman's BTU expenditure to accomplish his respective EVA tasks, a PLSS expendable red line should not be reached during the EVA. The Commander is expected to expead approximately 3625 BTU's which will leave a 1175 BTU PLSS reserve or approximately 50 minutes Lunar surface time. (Metabolic profiles are presented in the Appendix, Section 5.4) In addition to the nominal timeline, the plan presents three other timelines for the lunar EVA. One timeline is referred to as an alternate timeline and two are referred to as contingent timelines. These timelines differ from the nominal primarily by additions or deletions of tasks. The major difference in the alternate timeline, from the nominal, is the addition of the S-band erectable antenna deployment which reduces the time available for the documented sample collection. The first contingent timeline, Contingent EVA 1, is a presentation of activities for a minimum-time, one-man EVA. The second contingent timeline, Contingent EVA 2, is for a one-man, two-hour EVA. . �The p l a n a l s o p r e s e n t s two forms of t i m e l i n e s . The l i n e s and a t i m e l i n e f o r t h e complete l u n a r s u r f a c e touchdown t o l i f t o f f , a r e i n summary form. Each of t i m e l i n e s i s a l s o p r e s e n t e d i n an expanded t i m e l i n e v i a t e d procedures form. EVA times t a y , from t h e EVA and abbre- D e t a i l e d procedures a r e included f o r t h e nominal l u n a r EVA. S i n c e t h e a l t e r n a t e t i m e l i n e , i n g e n e r a l , only adds t h e deployment of t h e e r e c t a b l e antenna and reduces t h e time f o r c o l l e c t i o n of a documented sample, d e t a i l e d procedures f o r t h e e n t i r e a l t e r n a t e EVA would b e redundant. Thus, only d e t a i l e d procedures f o r t h e S-band e r e c t a b l e antenna deployment a r e included. For t h e c o n t i n g e n t EVA'S, t h e t i m e l i n e s p r e s e n t t h e procedures i n s u f f i c i e n t d e t a i l t h a t , with a n understanding o r r e f e r e n c e t o t h e nominal procedures, s e p a r a t e procedures a r e unnecessary. �SECTION 2.0 MISSION PLAN �MISSION PLAN Mission Purpose The primary purpose of t h e Apollo 11 mission i s t ~ ' ~ e r f o r m a manned l u n a r landing and r e t u r n . Subordinate o b j e c t i v e s a r e t o perform l i m i t e d s e l e n o l o g i c a l i n s p e c t i o n , photography, survey, e v a l u a t i o n , and sampling during t h e l u n a r s t a y . Data w i l l b e obtained t o a s s e s s t h e c a p a b i l i t y and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment i n t h e l u n a r environment. The accomplishment of t h e d e t a i l e d l u n a r s u r f a c e mission' o b j e c t i v e s and experiments w i l l c o n t r i b u t e a n e s s e n t i a l p a r. t . t o t h e success of t h e mission. 2.2 Mission Description This s e c t i o n provides a b r i e f summary of t h e major events f o r a J u l y 16, 1969 launch date. Launch t o Earth Orbit: The J u l y 16 mission w i l l allow a range of launch azimuths from 72 t o 108 degrees with a window opening a t 13:32:00 The s p a c e c r a f t (hr:min:sec) gmt f o r a d u r a t i o n of 4:24:00. w i l l b e i n s e r t e d i n t o an approximately 100 n a u t i c a l m i l e c i r c u l a r e a r t h parking o r b i t f o r s p a c e c r a f t checkout. Translunar I n j e c t i o n (TLI) : The J u l y window permits a P a c i f i c t r a n s l u n a r i n j e c t i o n . The S-IVB w i l l b e re-ignited during t h e second e a r t h p a r k i n g o r b i t t o provide t h e nominal i n j e c t i o n . Translunar Coast: Two hours a f t e r TLI, t h e CSM w i l l s e p a r a t e from t h e S-IV, transpose, dock and i n i t i a t e e j e c t i o n of t h e LM/CSM. P r i o r t o l u n a r o r b i t i n s e r t i o n (LOI), two a s t r o n a u t s w i l l e n t e r t h e LM, accomplish a l i m i t e d s t a t u s check, and r e t u r n t o t h e command module. �Lunar Orbit Insertion: The service module propulsion system will insert the spacecraft into an orbit of approximately 60 by 170 nautical miles. After two revolutions in this orbit for spacecraft system and orbit parameter checks, the orbit will be reduced to 66 by 54 nautical miles.. Lunar Module Descent: During the thirteenth orbit after the Lunar Orbit ~nsertion, LM/CSM undocking is accomplished in preparation for lunar landing. The powered descent maneuver is initialized at pericynthion of the descent transfer orbit. For the July 16 launch, the lunar landing will be at Site 2 (previously designated 11-P-6 and located at 0" 43' N, 23" 42' E). The range of sun elevation angles, for landing, will be from 10.5 to 13.5 degrees. Lunar Surface Operations: The planned lunar surface staytime is 22 hours. The nominal plan provides for a single, two-man EVA, with a duration of two hours and forty minutes. . . . Immediately after landing, the LM will be checked to assess its launch capability. After the post-landing checks, there will be a four hour rest period, with eat periods before and after, prior to preparation for EVA. Following the EVA and post-EVA activities, there will be another rest period, of four hours and forty minutes duration, prior to preparation for liftoff. In addition to the tasks required to successfully complete the landing and.ascent and the pre-EVA and post-EVA operations, the lunar surface activities will include the following major items in order of priority: 1) Photographs of the landing area through the LM cabin window. 2) Contingency sample collection. �3) EVA e v a l u a t i o n . 4) LM i n s p e c t i o n . 5) Bulk sample c o l l e c t i o n . 6) Deployment of experiments : Early Apollo . S c i e n t i f i c Experiments Package (S-031, Lunar P a s s i v e Seismology and S-078, Laser Ranging Retro-Reflector) and S-080, S o l a r Wind Composition. 7) Documented sample c o l l e c t i o n . Real time TV coverage w i l l b e provided e a r l y i n t h e EVA u s i n g t h e s t e e r a b l e antenna o r , i f r e q u i r e d , t h e e r e c t a b l e antenna. Both t h e Goldstone and Parkes 210-foot antennas w i l l b e u t i l i z e d as a v a i l a b l e . Photography w i l l b e employed throughout t h e EVA t o document t h e a c t i v i t i e s and o b s e r v a t i o n s . LM A s c e n t : During t h e LM l u n a r s u r f a c e s t a y , t h e CSM w i l l make t h e r e q u i r e d p l a n e change t o permit a nominally coplanar rendezvous. A f t e r LM a s c e n t and docking t o t h e CSM, t h e two crewmen w i l l t r a n s f e r t o t h e CSM w i t h exposed f i l m and samples of t h e l u n a r s u r f a c e . The CSM w i l l then j e t t i s o n t h e LM u s i n g t h e SM RCS. Transearth Injection: The s e r v i c e module p r o p u l s i o n system w i l l b e used t o b o o s t t h e CSM o u t of l u n a r o r b i t . The r e t u r n f l i g h t d u r a t i o n s h a l l n o t exceed 110 hours and t h e r e t u r n i n c l i n a t i o n s h a l l n o t exceed 40 degrees. Entry and Recovery: P r i o r t o atmospheric e n t r y , t h e command module w i l l b e s e p a r a t e d from t h e s e r v i c e module u s i n g t h e SM RCS. The nominal range from 400,000 f e e t a l t i t u d e t o touchdown s h a l l b e 1285 n a u t i c a l miles.. Touchdown w i l l be i n t h e P a c i f i c n e a r Hawaii approximately 11 days a f t e r launch from e a r t h . �P o s t Landing Operations: Following splashdown, t h e crew w i l l e g r e s s t h e CM a f t e r t h e f l o t a t i o n c o l l a r h a s been a t t a c h e d , don b i o l o g i c a l i s o l a t i o n garments, t r a n s f e r t o t h e recovery s h i p by h e l i c o p t e r and immediately e n t e r t h e Mobile Quarantine F a c i l i t y (MQF) They w i l l b e t r a n s p o r t e d i n t h e MQF t o t h e LRL a t MSC. The CM, sample r e t u r n c o n t a i n e r s , f i l m , t a p e s and a s t r o n a u t l o g s w i l l a l s o b e t r a n s p o r t e d t o t h e LRL. . I n o r d e r t o minimize t h e r i s k of contamination of t h e e a r t h ' s b i o s p h e r e by l u n a r m a t e r i a l , q u a r a n t i n e measures w i l l b e enforced. The crew w i l l b e q u a r a n t i n e d f o r approximately 2 1 days a f t e r l i f t o f f from t h e l u n a r s u r f a c e . 2.3 Summary of Mission Requirements 2.3.1 Introduction The f o l l o w i n g i n f o r m a t i o n i s from t h e "Mission Requirements SA-506lCSM-107lLM-5 G Type Mission, Lunar Landing", Dated A p r i l 17, 1969. (Revised May 1, 1969) The f o l l o w i n g s i n g l e primary mission o b j e c t i v e i s a s s i g n e d t o t h i s . m i s s i o n by t h e O f f i c e of Manned Space F l i g h t (OMSF): 1) Perform manned l u n a r l a n d i n g and r e t u r n . I n a d d i t i o n , t h e f o l l o w i n g s u b o r d i n a t e o b j e c t i v e s a r e del i n a t e d by OMSF: 1) P e r f orm s e l e n o l o g i c a l i n s p e c t i o n and sampling. 2) Obtain d a t a t o a s s e s s t h e c a p a b i l i t y and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment i n t h e l u n a r s u r f a c e environment. F i n a l l y , t h e f o l l o w i n g experiments have been a s s i g n e d t o t h i s mission: 1) S-031 Lunar P a s s i v e Seismology 2) S-078 L a s e r Ranging Retro-Reflector �. . 3) S-080 S o l a r Wind Composition 4) S-151 Cosmic Ray Detection 5) T-029 P i l o t Describing Function . . . . . The Mission Requirements document i n c o r p o r a t e s t h e s e v a r i o u s o b j e c t i v e s and experiments, d e t a i l s them where necessary, and places them i n t h e proper order of p r i o r i t y , thereby providing t h e l e v e l of d e t a i l necessary f o r mission planning. The document n o t e s , however, t h a t : . There a r e no Detailed Objectives, a s such, which have been derived from t h e primary o b j e c t i v e of "perform manned l u n a r landing and return"., D e t a i l e d Objectives have, however, been derived from t h e two OMSF subordinate o b j e c t i v e s . The mission w i l l b e flown as an o p e r a t i o n a l mission i n t h e sense t h a t i t w i l l b e performed i n t h e most expeditious manner p o s s i b l e with no i n t e r f e r e n c e from s p e c i a l tests o r operations which a r e n o t necessary f o r t h e performance of t h i s b a s i c o b j e c t i v e . The manner i n which t h e detailed.performance of t h i s o b j e c t i v e i s met w i l l be contained i n t h e Mission Report. 2) Experiments a r e d e t a i l e d and p r i o r i t i e d i n t h e requirements document only when they a r e such a s t o r e q u i r e some a c t i o n by t h e crew o r otherwise impact t h e timeline. Thus, t h e Cosmic Ray Detection experiment, S-151, a passive experiment l i m i t e d t o p o s t mission a n a l y s i s of t h e f l i g h t helmets, is only mentioned and does n o t appear i n t h e p r i o r i t y list o r a s a detailed objective. S i m i l a r l y , ' t h e P i l o t Describing Function experiment, T-029, only r e q u i r e s c e r t a i n p o r t i o n s of voice and telemetry d a t a recordings and does n o t appear i n t h e l i s t of o b j e c t i v e s and experiments. The Detailed Objectives f o r t h e f i r s t l u n a r landing mission w i l l b e o b j e c t i v e s which concern equipment and crew o p e r a t i o n s only during t h e l u n a r surf ace phase of t h e mission. The c a p a b i l i t y t o s u c c e s s f u l l y complete o t h e r mission phases w i l l have been demonstrated on p r i o r missions. �Mission O b j e c t i v e s and Experiments .The f o l l o w i n g summary of l u n a r EVA o b j e c t i v e s and experiments i s i n o r d e r of p r i o r i t y , w i t h t h e o b j e c t i v e o r experiment of h i g h e s t p r i o r i t y l i s t e d f i r s t . The o r d e r of p r i o r i t y i s based upon t h e r e l a t i v e importance t o t h e Apollo s p a c e c r a f t development program o r t o t h e advancement of l u n a r s c i e n c e . The D e t a i l e d O b j e c t i v e s and Experiments a r e i n c l u d e d i n t h e Appendix, S e c t i o n 5.2. The o b j e c t i v e s " T e l e v i s i o n Coverage" and "Photographic Coverage" w i l l b e performed i n c o n j u n c t i o n w i t h s e v e r a l of t h e o t h e r obj e c t i v e s o r experiments. The a s s o c i a t e d o p e r a t i o n s w i l l t a k e p l a c e a t v a r i o u s p o i n t s i n t h e t i m e l i n e . Hence, t h e s e two ' o b j e c t i v e s cannot b e a s s i g n e d any s p e c i f i c p r i o r i t y i n t h e l i s t below and a r e t h e r e f o r e i n c l u d e d a t t h e end. Priority O b j e c t i v e s and Experiments 1 A Contingency Sample C o l l e c t i o n B Lunar S u r f a c e EVA Operations 3 C EMU Lunar Surface Operations 4 D Landing E f f e c t s on LM 5 E Lunar S u r f a c e C h a r a c t e r i s t i c s 6 F Bulk Sample C o l l e c t i o n 7 G Landed LM Location 8 H Lunar Environment V i s i b i l i t y 9 I Assessment of Contamination by Lunar M a t e r i a l 10 S-031 Lunar P a s s i v e Seismology 11 S-078 Laser Ranging Retro-Reflector 12 S-080 S o l a r Wind Composition �J Documented Sample C o l l e c t i o n K (Included i n Photographic Coverage, Change A, May 1, 1969) L T e l e v i s i o n Coverage M Photographic Coverage �SECTION 3.0 NOMINAL LUNAR EVA �' . 3.0 NOMINAL LUNAR EVA 3.1 Timeline D e s c r i p t i o n and Rationale 3.1.1 Lunar Surface Stay The nominal plan i s f o r two crewmen, t h e Commander and t h e Lunar Module P i l o t , t o remain on t h e l u n a r s u r f a c e f o r approximately 22 hours. During t h i s period, the'crew w i l l accomplish postlanding and pre-ascent procedures and e x t r a v e h i c u l a r a c t i v i t y . There w i l l be two r e s t and s e v e r a l e a t periods. A timeline f o r t h e l u n a r s u r f a c e s t a y i s presented i n Figure 3-1. There a r e s e v e r a l c o n s i d e r a t i o n s which a r e t h e b a s i s f o r t h e sequence of a c t i v i t y f o r t h e l u n a r s u r f a c e s t a y . An e a r l y r e s t peiod i s planned which w i l l provide r e s t b e f o r e t h e strenuous pre-EVA, EVA, and post-EVA a c t i v i t i e s and i n s u r e t h e work day i s n o t p r o h i b i t i v e l y long i f l i f t o f f i s req u i r e d b e f o r e t h e o t h e r planned r e s t period. A second r e s t p e r i o d of f o u r hours and f o r t y minutes i s provided a f t e r t h e EVA b e f o r e t h e c r u c i a l l i f t o f f and rendezvous sequence. 3.1.2 - Extravehicular A c t i v i t y The f i r s t l u n a r EVA i s designed t o maximize t h e r e t u r n of s c i e n t i f i c and o p e r a t i o n a l data. However, t h e t i m e l i n e permits r e s t periods and a gradual i n c r e a s e i n t a s k complexity w i t h simple t a s k s i n i t i a l l y f o r crew acclimation and PLSS-EMU data analysis. There w i l l be two major a r e a s of e v a l u a t i o n during t h e l u n a r s u r f a c e EVA. The f i r s t concern i s with comprehensive crew f a m i l i a r i z a t i o n and e v a l u a t i o n of EVA c a p a b i l i t y and t h e l u n a r environment. The i n v e s t i g a t i o n w i l l b e a methodical approach which w i l l enhance t h e accomplishment of t h i s EVA a s w e l l a s demonstrate a s t r o n a u t and equipment c a p a b i l i t y f o r f u t u r e l u n a r s u r f a c e e x p l o r a t i o n . The second a r e a is t h e c o l l e c t i o n of o p e r a t i o n a l and s c i e n t i f i c data. The a n a l y s i s of t h i s d a t a w i l l a s s i s t i n t h e update of equipment designs a s ' w e l l a s i n c r e a s e our general understanding of t h e l u n a r s u r f a c e . The f i r s t few minutes of t h e EVA; t h e Lunar Module P i l o t (LMP) w i l l remain i n s i d e t h e LM a s c e n t s t a g e t o monitor t h e Commander's (CDR) s u r f a c e a c t i v i t y and t h e LM systems i n t h e �' depressurized state. The CDR will descend to the lunai surface to conduct several preliminary tasks. He will determine . his ability to operate in the lunar environment; collect a contingency lunar sample and take still color photographs (with an electric 70mm camera) as he checks the LM . and the lunar surface condition which affect the accomplishment of the EVA tasks. In addition to the TV coverage and still photographs, the LMP can visually observe and obtain sequence camera (data acquistiion) coverage to supplement the documentation of the CDR activity. With only one crewman on the surface during the first few minutes of the EVA, a more effective PLSS telemetry data analysis can be conducted. The real time use rate for the PLSS consumables will be compared with the predicted rate to determine the PLSS capability for'EVAcontinuation. After the CDR accomplishes the preliminary EVA tasks, the LMF' will descend to the surface and spend a few minutes in the familiarization and evaluation of his capability or limitations to conduct further operations in the lunar environment. After this short period of time he will deploy the Solar Wind Composition (SWC) experiment. The CDR, after photographing the LMPts egress and descent to the surface, will remove the TV camera and tripod from the descent for stage modularized equipment stowage assembly (MESA) and move them to a position for optimum coverage of the subsequent surface EVA operations. Then, while the CDR collects a bulk sample of lunar surface material, the LMP will continue to become more familiar with his ability to operate in the lunar environment as he conducts the EVA and Environment Evaluation. The LMP begins the LM inspection and is joined by the CDR after the bulk sample has been collected. When the crewmen reach the scientific equipment (SEQ) bay in Quad 11, the LMP removes the Early Apollo Scientific Experiments Package (EASEP) as the CDR completes the LM inspection and photographically documents the LMP's activity. After they deploy the EASEP, the crew will select, describe, photograph, and collect samples until they terminate the EVA. In summary, there is a general increase in task complexity for both crewmen. The conservative timeline permits the crew to follow a slow, methodical approach in accomplishing each task. Additionally, the frequent rest periods within �Figure 3 - 1 rum scrlr )r,Ono f:LY."ct KCM !LY Q -;I -2 IM MRS. -13 w fZccml UIPOSKIIC V . 4 UI COYWLMEU k PILOT ACTIVITY <> T I M SCAlr IYHRS.-3 -:z 'I 0 A TO~W W N OYISIDI lWlNEml .C*ICKWI ~CO C II~C IV 4 w wurcff n s m n C l U L C10lI C M l W U l D l H A M 1 OI?RESS O e t t P L t E E W I P U f I l PC4 J E I I I S O I Y Y P L C CDLLECllm OREIIYIUtVCMCCIS . S d l l D I ~ 1 t I M D C I L O V Y I ~ l U L l E * M l E ISYC LINE1 O L Y I I#IlUL CVAA.OEWIOYEIl4L CAY. 01" .I0 s 1 C OIPLWY.1 OW. E I V l t O l f I1W U W I I O I .-LI Y Y I L E COLLCCIDI U I IISP(ClIO# .EASE, OCPLOVYE*I *XXUYE#lCO Y Y P L E ICM U I SUT I 111EGtllV .Jf111SOm EWI* ~ S l A B L I S *c.11" I.1ICtllV �LUNAR SURFACE ACTIVITY TIMELINE FOR 22 HOUR STAY 1 tuaw ! t I i t srArus cmm 1I WRM U CLfll 8 ?~~CWnWllW I 1 061VE GO $01 RE51 �t h e timeline add t o t h i s conservatism and i n s u r e t h a t each crewman and h i s PLSS remain i n a nominal o p e r a t i n g condition. However, should t h e EVA b e terminated a t any p o i n t i n t h e t i m e l i n e , t h e maximum d a t a r e t u r n f o r t h e t i m e spent on t h e . s u r f a c e w i l l be assured. Task and Data Descriptions Although t h e d e t a i l e d procedures d e s c r i b e t h e s t e p s t o ac- ,complish each t a s k , f u r t h e r explanation of t h e d e s i r e d d a t a and d a t a c o l l e c t i o n processes is d e s i r a b l e . 3.2.1 Environmental F a m i l i a r i z a t i o n A s mentioned previously, t h e t i m e l i n e considerations f o r t h e l u n a r s u r f a c e e x t r a v e h i c u l a r a c t i v i t y w i l l permit a slow buildup of t a s k complexity t o i n s u r e thorough crew f a m i l i a r i z a t i o n with t h e l u n a r environment y e t optimize t h e d a t a r e t u r n . The approach with which t h e crewmen w i l l proceed w i l l permit them t o adapt t o t h e environment while determining t h e ease o r d i f f i c u l t y which they can expect through o u t t h e EVA. The f i r s t crewman t o e g r e s s , a f t e r determining h i s i n i t i a l EVA c a p a b i l i t y , can a d v i s e t h e second crewman on what t o expect and possibly suggest methods t o accomplish t h e a d d i t i o n a l t a s k s . Both crewmen's experiences w i l l b e invaluable f o r p r e d i c t i n g crew c a p a b i l i t y on f u t u r e l u n a r s u r f a c e explorations. Once on t h e s u r f a c e , t h e CDR w i l l move slowly from t h e footpad t o check h i s balance and determine h i s a b i l i t y t o cont i n u e with t h e EVA--the a b i l i t y t o move and t o s e e o r , s p e c i f i c a l l y , t o perform t h e s u r f a c e operations w i t h i n t h e c o n s t r a i n t s of t h e EMU and t h e l u n a r environment. Although a more thorough e v a l u a t i o n and documentation of a.crewmanls c a p a b i l i t i e s w i l l occur l a t e r i n t h e timeline, t h i s i n i t i a l f a m i l i a r i z a t i o n w i l l a s s u r e t h e CDR t h a t h e and t h e LMP a r e capable of accomplishing t h e assigned EVA t a s k s . Also, should i t be necessary t o unexpectedly terminate t h e EVA p r i o r t o f u r t h e r environment evaluation, t h i s e a r l y famili a r i z a t i o n w i l l i n s u r e some d a t a r e t u r n on EVA c a p a b i l i t y and t h e l u n a r s u r f a c e p r o p e r t i e s . �. 3.2.2 . P r e l i m i n a r y Checks For t h e P r e l i m i n a r y Checks t h e CDR w i l l t r a n s f e r t h e 70mm . EL Data.camera t o t h e s u r f a c e , conduct a b r i e f LM check and a p r e l i m i n a r y e v a l u a t i o n of t h e l u n a r environment. The Hasselblad camera w i l l e n a b l e t h e CDR t o t a k e s t i l l c o l o r photographs t o supplement t h e sequence ( d a t a a c q u i s i t i o n ) camera photography which t h e LMP w i l l a t t a i n through t h e LM a s c e n t s t a g e window t o document.the s u r f a c e a c t i v i t y . A b r i e f check of t h e LM s t a t u s i s a simple t a s k which can b e used t o extend t h e CDR's environment f a m i l i a r i z a t i o n . and, a t t h e same time, p r o v i d e an important c o n t r i b u t i o n ' t o t h e p o s t f l i g h t assessment of t h e LM l a n d i n g should a . f u l l o r nominal LM i n s p e c t i o n n o t b e accomplished l a t e r . The p r e l i m i n a r y e v a l u a t i o n of t h e c o n d i t i o n s which w i l l . i n f l u e n c e t h e crewmen's s u r f a c e o p e r a t i o n s , such a s t h e t e r r a i n s u r f a c e f e a t u r e s and l i g h t i n g o r v i s i b i l i t y , w i l l a l s o enhance t h e CDR's environmental f a m i l i a r i z a t i o n 'as w e l l a s h i s assessment of an a s t r o n a u t ' s c a p a b i l i t y t o accomplish EVA t a s k s . From a p o s i t i o n n e a r t h e l a d d e r t h e CDR w i l l make a g e n e r a l i n s p e c t i o n of t h e LM and s u r f a c e about t h e LM. For t h e LM and s u r f a c e v i s i b l e t o him, h e w i l l b r i e f l y examine t h e g e a r s t r u t s , f o o t p a d s , and major p a r t s of t h e s p a c e c r a f t t o a s s u r e t h a t t h e LM i s s t a b l e and w i l l provide a s a f e o p e r a t i o n s b a s e f o r t h e l u n a r s t a y . An i n s p e c t i o n of t h e s u r f a c e w i l l prov i d e p r e l i m i n a r y d a t a on t h e LM e f f e c t on t h e s u r f a c e d u r i n g t h e landing. 3.2.3 TV Coverage The primary purpose of t h e TV i s t o provide a supplemental r e a l time d a t a s o u r c e t o a s s u r e o r enhance t h e s c i e n t i f i c and o p e r a t i o n a l d a t a r e t u r n . It may b e a n a i d i n d e t e r mining t h e e x a c t LM l o c a t i o n on t h e l u n a r s u r f a c e , i n e v a l u a t i n g t h e EMU and man's c a p a b i l i t i e s i n t h e l u n a r environment and i n documenting t h e sample c o l l e c t i o n s . The TV w i l l b e u s e f u l i n p r o v i d i n g continuous o b s e r v a t i o n f o r time c o r r e l a t i o n of crew a c t i v i t y w i t h t e l e m e t e r e d d a t a , v o i c e comments, and photographic coverage. �TV r e c e p t i o n , w i t h o u t a d e g r a d a t i o n of b o t h v o i c e and t e l e metered i n f o r m a t i o n , may b e dependent on having t h e LM s t e e r a b l e S-band antenna r a d i a t e t o a 210-foot antenna, e i t h e r t h e Goldstone ( C a l i f o r n i a ) o r t h e Parkes ( A u s t r a l i a ) antenna, o r deploy t h e S-band e r e c t a b l e antenna on t h e l u n a r s u r f a c e . (A comparison of t h e performance expected w i t h t h e 210-foot/ s t e e r a b l e antennas o r 8 5 - f o o t / e r e c t a b l e antennas i s p r e s e n t e d i n T a b l e 3-1 on t h e f o l l o w i n g page.) The e r e c t a b l e antenna makes i t p o s s i b l e t o r e c e i v e TV t r a n s m i s s i o n s w i t h t h e 85-foot antenna d i s h e s a t e i t h e r Goldstone, Madrid, o r Canberra, which a r e e q u i v a l e n t t o t h e 2 1 0 - f o o t / s t e e r a b l e combination. I f a 210-foot antenna i s n o t i n view o r t h e e r e c t a b l e antenna has n o t been deployed, TV coverage may b e o b t a i n e d by a c c e p t i n g t h e l o s s ' o r d e g r a d a t i o n of v o i c e a n d t e l e m e t r y . The f i n a l d e c i s i o n f o r such coverage w i l l b e made i n r e a l t i m e and based on t h e q u a l i t y of t h e communications up t o . . that point. . . ' .:. - For t h e nominal mission, w i t h a J u l y 16 launch d a t e , t h e Goldstone and/or t h e Parkes antennas w i l l b e i n v i e w ' d u r i n g t h e EVA. The coverage provided by t h e 210-foot and 85-foot antennas d u r i n g t h e l u n a r s t a y i s shown i n ~ i g u r e . 3 - 2 . The TV camera w i l l have two primary p o s i t i o n s ' o r f i e l d s of view . f o r coverage of t h e s u r f a c e ' a c t i v i t y . The camera w i l l b e mounted i n ' t h e descent s t a g e Modularized Equipment Stowage Assembly (MESA) t o view ' t h e crewmen's d e s c e n t t o t h e s u r f a c e and t h e CDR's ' a c t i v i t y i n t h e immediate l a d d e r a r e a . (See Figure 3-3). A f t e r t h e LMP'S descent t o ' t h e s u r f a c e , t h e CDR removes t h e camera and t r i p o d from t h e MESA and p l a c e s t h e t r i p o d w i t h camera on t h e s u r f a c e i n an optimum p o s i t i o n ' f o r coverage of subsequent s u r f a c e a c t i v i t y . (See F i g u r e 3-4). �TABLE 3-1 (EM .Mode -~ i Power) ~ h 210 '. MARS STAT1ON 85' MSFN STATION NOMINAL WORST CASE NOMINAL WORST CASE +15.4 +25.4 +23.4 + 7.2 + 1.8 +17.2 +15.2 +11.8 + 9.8 + 7.7 +17.7. E r e c t a b l e Antenna + 8.8 + 9.2, 51.2 kbps Telemetry*" . . EVA Voice (dual) dB EVA EKG & PLSS Data (dual) +.3.8 . . + 9.7 . . T e l e v i s i o n (B&W) . 1.6 kbps Telemetry** +17.4 EVA Voice (dual) + 9.2 + 3.8 + 9.7 EVA EKG & PLSS Data . (dual) ~ e l e v ii so n (B&w) ' S t e e r a b l e Antenna . . . . 51.2 kbps Telemetry** .' EVA Voice (dual) EVA EKG & PLSS Data (dual) + 0.7 - + 1.1 - 4.3 - 1.1 - 6.5 - 0.6 +7.1 EVA Voice (dual) EVA EKG & PLSS Data (dual) - .4.3 - 6.5 T e l e v i s i o n (B&W) + 1.6 - 0.6 1.6 kbps' Telemetry** . . +17.3 + 3.7 + 9.6 +'6.5 + 6.9 . + 1.5 + 7.4 ' +15.1 + 1.5 + 7.4 ' . Based on measured LM-5 'data and MSC t e s t . d a t a on new. (1969) Motorola FM demodulator. The MSC t e s t s were conducted i n t h e ISD E l e c t r o n i c Systems T e s t F a c i l i t y (on one u n i t ) . ' ** + 8.7 + 9.1 + 3.7 + 9.6 1.5 + 1.6 + 9.3 + 1.1 T e l e v i s i o n . (B&W) * +15.7 . For a BER bf . . 16 ' �-16 . 0 .20 J U I 20 ~ 4 8 12 J U ~ Y21 16 20 Greenwich mean time, G a t .~ . . hr. : Figure 3-2.'- Radar coverage during lunar stay f o r launch date of July 16. 0 4 JU~Y 22 �"Z" - plane - / ~ i e wnormal cenl:er line Figure 3-3. - TV field of view from MESA. 18 �Figure 3-4 .-TV field of view from tripod (with Lunar day lens) 18a �3.2.4 S-Band E r e c t a b l e Antenna Deployment ( A l t e r n a t e Timeline) The S-band e r e c t a b l e antenna w i l l be deployed t o i n c r e a s e t h e communications c a p a b i l i t y . I t ' s major impact t o t h e EVA i s i n o b t a i n i n g an e q u i v a l e n t communications c a p a b i l i t y t h a t w i l l b e p o s s i b l e otherwise only i f a 210-foot antenna i s i n view. This communications c a p a b i l i t y may be r e q u i r e d f o r simultaneous TV, v o i c e , and t e l e m e t e r e d d a t a r e t u r n . (See t h e d i s c u s s i o n on t h i s s u b j e c t i n t h e previous s e c t i o n on TV coverage, S e c t i o n 3.2.3). ' . ,, . 3.2.5 The deployment of t h e e r e c t a b l e antenna i s a time-consuming task--deployment time i s expected t o be 19 minutes. However, t h e TV c o v e r a g e , ' w i t h o u t a d e g r a d a t i o n of v o i c e and t e l e m e t r y , gained through t h e use of t h e antenna may r e q u i r e i t t o be deployed. I n t h i s s i t u a t i o n , although i t i s d e s i r a b l e t o a t t a i n t h i s advantage provided by t h e antenna and t o p e r m i t t h e crewman i n s i d e t h e LM t o switch t o t h e e r e c t a b l e antenna e a r l i e r i n t h e t i m e l i n e , t h e crewman's f a m i l i a r i z a t i o n w i t h l u n a r o p e r a t i o n s b e f o r e t h i s p o i n t i s considered t o b e i n s u f f i c i e n t t o s a f e l y and e f f e c t i v e l y accomplish the' deployment task. Photography photography, s t i l l c o l o r photographs w i t h t h e 70mm EL d a t a camera, close-up s t e r e o photographs w i t h t h e Apollo Lunar S u r f a c e Close-up Camera (ALSCC), and motion p i c t u r e s w i t h t h e 16mm ( d a t a a c q u i s i t i o n ) camera, w i l l be a v i t a l p a r t of t h e d a t a c o l l e c t i o n p r o c e s s f o r t h e EVA. A 70mm camera, w i t h b l a c k and w h i t e f i l m , w i l l b e used f o r ' s u r f a c e photography from t h e LM and w i l l b e t r a n s f e r r e d t o ' t h e s u r f a c e . . i f a m a l f u c t i o n of t h e o t h e r camera occurs. . . The crewmen w i l l u s e t h e EL d a t a camera e x t e n s i v e l y on t h e s u r f a c e t o document each major t a s k which they accompl i s h . A d d i t i o n a l photography, such a s panoramas and s c i e n t i f i c documentation, w i l l supplement o t h e r d a t a i n t h e p o s t f l i g h t a n a l y s i s of t h e l u n a r environment and t h e a s t r o n a u t ' s c a p a b i l i t i e s o r l i m i t a t i o n s on conducting l u n a r s u r f a c e o p e r a t i o n s . With t h e ALSCC t h e crewmen may photograph a r e a s of , t h e l u n a r surface not disturbed during t h e landing o r surface a c t i v i t y , t h e i r f o o t p r i n t s , a r e a s a f f e c t e d by t h e LM footpads and t h e s c i e n t i f i c equipment, and o t h e r phenomena of o p e r a t i o n a l and' scientific interest. �The sequence camera, from t h e LM a s c e n t s t a g e window, w i l l p r o v i d e almost continuous coverage of t h e s u r f a c e a c t i v i t y . The Lunar Module P i l o t , who remains i n s i d e t h e a s c e n t s t a g e f o r t h e f i r s t few minutes of t h e EVA, w i l l u s e t h e seauence camera t o document t h e Commander's i n i t i a l s u r f a c e a c t i v i t i e s . Then, b e f o r e h e e g r e s s e s , t h e LMP w i l l p o s i t i o n t h e camera f o r optimum s u r f a c e coverage w h i l e b o t h crewmen a r e on t h e s u r f a c e . And, a f t e r t h e LMP i n g r e s s e s , h e can u s e t h e sequence camera t o p r o v i d e coverage of t h e remaining s u r f a c e activity. A complete d e s c r i p t i o n of t h e camera equipment and t h e i r operat i o n a l procedures, a s w e l l as t h e d e t a i l s of t h e documentation provided by t h e t h r e e cameras, a r e contained i n Reference 6 . 3.2.6 EVA and Environment Evaluation The primary purpose of t h e Environmental F a m i l i a r i z a t i o n p e r i o d , e a r l y i n t h e t i m e l i n e , i s t o allow t h e crew s u f f i c i e n t time t o adapt t o t h e new environment and o p e r a t i n g c o n d i t i o n s . The EVA and Environment E v a l u a t i o n , however, i n v o l v e s a d e t a i l e d i n v e s t i g a t i o n and documentation of a crewman's c a p a b i l i t y w i t h i n t h e c o n s t r a i n t s of t h e EMU, t h e PLSSIEMU performance under v a r y i n g c o n d i t i o n s of s u n l i g h t , shadow, crewman a c t i v i t y o r i n a c t i v i t y , and t h e c h a r a c t e r i s t i c s of t h e l u n a r environment which i n f l u e n c e o p e r a t i o n s on t h e s u r f a c e . The p r e l i m i n a r y f a m i l i a r i z a t i o n w i l l be of t h e most b e n e f i t i n r e a l time--to p r e p a r e t h e crewmen t o o p e r a t e d u r i n g t h i s EVA. On t h e o t h e r hand, t h e EVA and Environment E v a l u a t i o n p e r i o d should b e of s i g n i f i c a n t v a l u e f o r f u t u r e l u n a r s u r f a c e e x p l o r a t i o n . From t h e assessment of d a t a g a t h e r e d d u r i n g t h i s p e r i o d , s u f f i c i e n t knowledge should b e gained t o acc u r a t e l y p r e d i c t t h e c a p a b i l i t i e s and l i m i t a t i o n s of t h e a s t r o n a u t and h i s equipment f o r f u t u r e l u n a r s u r f a c e e x t r a vehicular activity. During t h e EVA and Environment E v a l u a t i o n t h e LMF w i l l determine, i n d e t a i l , t h e combined e f f e c t s of t h e EMU c o n s t r a i n t s and l u n a r g r a v i t y on h i s p h y s i c a l c a p a b i l i t i e s . H e w i l l compare h i s c a p a b i l i t i e s i n t h i s l u n a r environment w i t h s i m i l a r experiences d u r i n g e a r t h g r a v i t y and s i m u l a t e d l u n a r g r a v i t y e x e r c i s e s . He w i l l observe how t h e l u n a r s u r f a c e i s a f f e c t e d by t h e a c t i o n s he performs and c a r e f u l l y examine . t h e t e r r a i n t o determine t h e s u r f a c e c h a r a c t e r i s t i c s . Also, h e w i l l determine h i s v i s u a l p e r c e p t i o n of t h e s u r f a c e f e a t u r e s and h i s v i s u a l a c u i t y w i t h i n t h e c o n s t r a i n t s of t h e e x t r a v e h i c u l a r v i s o r assembly (EWA). �3.2.7 Sample Collections The nominal plan is to conduct three sample collections of lunar surface material. They are, in order of priority, the contingency, the bulk, and the documented sample collections. The contingency sample collection is a simple task which can be accomplished within a few minutes early in the EVA timeline. This will assure the'return of a small sample in a contingency situation where a crewman may remain on the surface for only a short period of time. One to two kilograms .of loose material will be collected near the LM ladder and the sample bag restowed in the suit pocket to be carried into the ascent stage when the crewman ingresses. In the bulk sample collection at least 10 kilograms of unsorted surface debris and selected rock chunks'willbe placed in a special container, an Apollo Lunar Sample Return Container (sRC), to provide a near vacuum environment for its Apollo return to the Lunar Receiving Laboratory (LRL). Lunar Handtools (ALHT), stowed in the MESA with the SRC, will be used to collect this large sample (30 to 60 pounds) of loose lunar material from the surface near the MESA in Quad IV of the LM. As each rock sample or scoop of loose material is collected it will be placed into a large sample bag. Placing the sealed bag, rather than the loose material directly into the SRC, also prevents contamination and possible damage to the container seals. The documented sample collection, like that of the bulk sample collection, will involve a large mass of lunar material placed into an SRC for return to earth: However, the documented sample will differ significantly in content and in its collection process. As the name implies the documented sample collection will involve the documentation of the individual samples and the area from which they are taken. It can be classified as a very limited lunar field geology investigation. �Within t h e documented sample c o l l e c t i o n a core t u b e sample i s f i r s t c o l l e c t e d t o p r o v i d e an a s e p t i c and s t r a t i f i e d sample n e a r t h e LM. A t a s i t e r e p r e s e n t a t i v e o f . t h e l a n d i n g a r e a , t h e crew w i l l examine, d e s c r i b e , photograph, and c o l l e c t rock fragments and l o o s e s u r f a c e m a t e r i a l samples and p l a c e them i n d i v i d u a l l y i n pre-numbered bags. ' T h e samples, i n t h e s m a l l bags numbered one through f o u r t e e n , a r e placed i n a l a r g e bag f o r t r a n s f e r t o and stowage i n t h e documented sample SRC. I f time p e r m i t s a f t e r c o l l e c t i n g t h e s m a l l bags of samples, t h e crew w i l l c o l l e c t two environment samples, r e p r e s e n t a t i v e of t h e b u l k sample, and a second c o r e t u b e sample. Additiona l l y , t h e l a r g e sample bag w i l l be f i l l e d , a s t h e b u l k sample bag, t o r e t u r n t h e maximum amount of s u r f a c e m a t e r i a l . The v a r i o u s samples w i t h i n t h e documented sample c o l l e c t i o n w i l l b e t a k e n from a r e a s n e a r t h e LM o u t t o p o s s i b l y 300 f e e t away. Although t h e l i m i t i n g d i s t a n c e from t h e LM f o r t h i s f i r s t s u r f a c e mission i s 300 f e e t , t h e r e a r e s e v e r a l reasons f o r t h e crew t o remain w i t h i n 100 f e e t . F i r s t , s i n c e t h e documented sample c o l l e c t i o n w i l l b e l a t e i n t h e EVA, t h e c a p a b i l i t y of t h e crew and t h e i r equipment w i l l b e l i m i t e d a t t h i s time. A d d i t i o n a l l y , on t h i s f i r s t l a n d i n g mission a r e l a t i v e l y cons e r v a t i v e approach i s necessary. Also, i t i s u n l i k e l y t h a t t h e t e r r a i n a t 300 f e e t w i l l be s i g n i f i c a n t l y d i f f e r e n t from t h e t e r r a i n w i t h i n 100 f e e t of t h e LM. 3.2.8 Lunar Module I n s p e c t i o n The purpose of t h e LM i n s p e c t i o n i s t o v i s u a l l y check and p h o t o g r a p h i c a l l y document t h e e x t e r n a l c o n d i t i o n of t h e LM a f t e r t h e f l i g h t t o t h e l u n a r s u r f a c e and t h e e f f e c t s of t h e LM l a n d i n g on t h e l u n a r s u r f a c e . The i n s p e c t i o n d a t a w i l l b e used t o v e r i f y t h e LM a s a s a f e and e f f e c t i v e v e h i c l e f o r l u n a r e x c u r s i o n s . The d a t a w i l l a l s o b e used t o g a i n more knowledge of t h e l u n a r s u r f a c e c h a r a c t e r i s t i c s . I n g e n e r a l ' t h e b e n e f i t of t h e . i n s p e c t i o n w i l l s e r v e t o advance t h e equipment d e s i g n and our understanding of t h e environment i n which i t operates. The crewmen w i l l methodically i n s p e c t and r e p o r t t h e s t a t u s of a l l e x t e r n a l p a r t s and s u r f a c e s of t h e LM which a r e v i s i b l e t o them. They w i l l examine t h e l u n a r s u r f a c e about t h e LM t o determine t h e i n t e r a c t i o n s of t h e LM footpads w i t h t h e l u n a r s o i l f o r s t u d y of t h e l u n a r s u r f a c e p r o p e r t i e s . The s t i l l c o l o r �photographs w i t h t h e Hasselblad and closeup cameras, w i l l supplement t h e i r v i s u a l documentation f o r p o s t f l i g h t engineeri n g a n a l y s i s and d e s i g n v e r i f i c a t i o n . They w i l l observe and photograph t h e Reaction C o n t r o l System (RCS) e f f e c t s on t h e LM, t h e l a n d i n g g e a r performance, t h e i n t e r a c t i o n s of t h e s u r f a c e and f o o t p a d s , and t h e Descent P r o p u l s i o n System (DPS) e f f e c t s on t h e s u r f a c e a s w e l l a s t h e g e n e r a l c o n d i t i o n of a l l . quadrants and l a n d i n g s t r u t s . (Refer t o F i g u r e s 3-5, 3 - 6 , 3-7, and 3-8 f o r t h e major LM i n s p e c t i o n p o i n t s .) 3.2.9 Experiment Deployments . . There a r e t h r e e s c i e n t i f i c experiments which w i l l ' b e deployed. The S o l a r Wind composition (SWC) experiment deployment, although of lowest p r i o r i t y , i s accomplished f i r s t a s i t is a s i m p l e t a s k and t h e r e s u l t s depend on t h e exposure time. A t l e a s t a n hour of exposure time i s d e s i r e d b e f o r e i t is p l a c e d i n a n SRC f o r r e t u r n t o e a r t h . The o t h e r two experiments, t h e P a s s i v e Seismic (PSE) and L a s e r Ranging R e t r o - r e f l e c t o r (LR3), a r e deployed l a t e r b u t w i l l c o n t i n u e t o r e t u r n d a t a a f t e r t h e mission. The SWC c o n s i s t s of a p a n e l of very t h i n aluminum f o i l r o l l e d and assembled i n t o a combination h a n d l i n g and deployment c o n t a i n e r . It i s stowed i n t h e MESA. Once t h e thermal b l a n k e t i s removed from around t h e ~ S equipment A i t is a s i m p l e t a s k t o remove t h e SWC, deploy t h e s t a f f and t h e f o i l "window shade", and p l a c e i t i n d i r e c t s u n l i g h t where t h e f o i l w i l l b e exposed t o t h e s u n ' s r a y s . The SWC i s designed t o e n t r a p n o b l e gas c o n s t i t u e n t s of t h e s o l a r wind, s u c h ' a s Helium, Neon, Argon, Krypton and Xenon. The f o i l is . l a t e r r o l l e d up, removed from t h e s t a f f , and placed i n an SRC. I f i t i s known a t t h e time t h e b u l k sample SRC i s packed t h a t a documented sample w i l l n o t b e c o l l e c t e d , t h e SWC w i l l b e p l a c e d i n t h e b u l k sample SRC. I f t h e b u l k sample SRC h a s been s e a l e d b e f o r e d e c i d i n g n o t t o c o l l e c t t h e documented sample t h e SWC may b e p u t i n t o t h e LMP's s u i t pocket f o r t r a n s f e r t o t h e a s c e n t s t a g e . A t t h e same t i m e t h e f o i l i s recovered, t h e a s t o n a u t w i l l push t h e s t a f f i n t o t h e l u n a r s u r f a c e t o determine, f o r p o s t f l i g h t s o i l mechanics a n a l y s i s , t h e depth of p e n e t r a t i o n . �Pad and surface descent stage Figure 3-5. - Quad I inspection points. Figure 3-6. - Quad II inspection points. 24 �S-band steerable antenna :ation Oxidizer pressurization Figure 3-7. - Quad III inspection points. S-band DPS effects on surface Figure 3-8. . - Quad I37 inspection points. �The PSE, o r t h e PSE package (PSEP), is one of two packages of t h e E a r l y Apollo S c i e n t i f i c Experiments Package (EASEP). It w i l l b e p l a c e d on t h e l u n a r s u r f a c e t o monitor l u n a r seismic a c t i v i t y and d e t e c t meteriod impacts, f r e e o s c i l l a t i o n s of t h e moon, and l u n a r i n t e r n a l a c t i v i t y . It may a l s o d e t e c t s u r f a c e deformations and v a r i a t i o n s of e x t e r n a l g r a v i t a t i o n a l f i e l d s a c t i n g on t h e moon. Data from t h i s s e l f c o n t a i n e d , solar-powered experiment package s h o u l d r e v e a l t h e p r o p e r t i e s of t h e s e i s m i c e v e n t s , t h e p h y s i c a l p r o p e r t i e s of t h e s u b s u r f a c e m a t e r i a l s , and t h e g e n e r a l s t r u c t u r e of t h e lunar interior. The LR3 i s a l s o one of t h e two EASEP packages. The package p r o v i d e s a c o r n e r r e f l e c t o r ( a c t u a l l y a n a r r a y of 100 r e f l e c t o r s ) f o r l a s e r ranging from e a r t h . From t h i s experiment t h e n a t u r e of t h e e a r t h ' s i r r e g u l a r r o t a t i o n may b e determined. Also, t h e d a t a w i l l h e l p r e f i n e t h e l u n a r motions and t h e r e l a t i v e motion of t h e e a r t h and moon. The PSEP and LR3 a r e on s e p a r a t e p a l l e t s which a r e stowed i n ' t h e S c i e n t i f i c Experiment (SEQ) bay of t h e d e s c e n t s t a g e Quad 11. I n t h e nominal deployment t h e LMP removes b o t h packages and c a r r i e s them t o t h e deployment s i t e simultaneously. 15 degrees The,crewmen w i l l s e l e c t a l e v e l s i t e , nominally w i t h i n of t h e LM -Y a x i s and 70 t o 110 f e e t from t h e LM. The s e l e c t i o n of t h e s i t e i s based on a compromise between a s i t e which minimizes t h e e f f e c t s of t h e LM a s c e n t e n g i n e d u r i n g l i f t o f f h e a t and contamination by d u s t and i n s u l a t i o n d e b r i s (kapton) from t h e LM d e s c e n t s t a g e , and a convenient s i t e n e a r t h e SEQ bay. + 3.2.10 U s e of t h e Lunar Equipment Conveyor The Lunar Equipment Conveyor (LEC) i s a d e v i c e which t h e a s t r o n a u t s w i l l u s e d u r i n g t h e EVA t o t r a n s f e r equipment t o o r from t h e a s c e n t s t a g e . It may a l s o b e used by t h e crewmen a s a s a f e t y t e t h e r when moving down t h e l a d d e r o r as a n a i d i n ascending t o t h e a s c e n t s t a g e . The LEC is a t h i n 60 fo-ot continuous loop of one i n c h wide s t r a p , which loops through a s u p p o r t p o i n t i n t h e a s c e n t s t a g e and back t o t h e crewman on t h e s u r f a c e . The end of t h e loop i s c l o s e d by two hooks, a t t a c h e d t o g e t h e r , which �p r o v i d e a means of s e c u r i n g equipment t o t h e LEC f o r t r a n s f e r . The crewman on t h e s u r f a c e can e f f e c t a t r a n s f e r t o t h e a s c e n t s t a g e by p u l l i n g t h e top s t r a p which causes equipment hooked t o t h e lower s t r a p t o move i n t o t h e a s c e n t stage. Although t h e t r a n s f e r of equipment with t h e LEC i s simple i n p r i n c i p l e , t h e a c t u a l t r a n s f e r o p e r a t i o n can r e q u i r e a s i g n i f i more i f c a u t i o n i s . n o t obc a n t amount of time and e f f o r t s e r v e d i n keeping t h e s t r a p s untangled o r i f t h e p r o p e r o p e r a t i o n a l procedures a r e n o t used. Because of t h e time involved (up t o f i v e minutes p l u s a r e s t p e r i o d ) , t h e number of equipment t r a n s f e r s i s k e p t t o a minimum. I n t h e nominal t i m e l i n e t h r e e t r a n s f e r s a r e planned, one t o t r a n s f e r t h e Hasselblad camera t o t h e s u r f a c e and one t r a n s f e r f o r each of t h e two SRC's. - EVA Termination For EVA t e r m i n a t i o n t h e r e a r e s e v e r a l advantages gained by one crewman i n g r e s s i n g b e f o r e an SRC i s t r a n s f e r r e d . ~ l t h o u g h i t i s p o s s i b l e t o t r a n s f e r an SRC i n t o t h e a s c e n t s t a g e b e f o r e t h e f i r s t crewman i n g r e s s e s , t h e crewman i n s i d e w i l l p r o v i d e some a s s i s t a n c e d u r i n g t h e t r a n s f e r . A d d i t i o n a l l y , h e w i l l remove t h e SRC and p l a c e i t where i t does n o t i n t e r f e r e w i t h i n g r e s s . The f i r s t crewman t o i n g r e s s w i l l a l s o make a LM system check, change t h e sequence camera f i l m magazine, and r e p o s i t i o n t h e camera t o cover t h e SRC t r a n s f e r and o t h e r crewman's l a d d e r a s c e n t . A s each man b e g i n s h i s EVA t e r m i n a t i o n h e w i l l c l e a n t h e EMU. Although t h e crew w i l l have a very l i m i t e d c a p a b i l i t y t o remove l u n a r m a t e r i a l from t h e i r EMU'S, they w i l l a t t e m p t t o brush o f f any d u s t o r p a r t i c l e s from t h e p o r t i o n s of t h e s u i t which they can reach and from t h e b o o t s on t h e footpad and l a d d e r . I n t h e EVA t e r m i n a t i o n t h e r e a r e two t a s k s which w i l l r e q u i r e some i n c r e a s e d e f f o r t . The f i r s t i s t h e a s c e n t from t h e . footpad t o t h e lowest l a d d e r rung. I n t h e unstroked p o s i t i o n t h e v e r t i c a l d i s t a n c e from t h e top of t h e footpad t o t h e lowest l a d d e r rung i s 31 i n c h e s . I n a nominal l e v e l l a n d i n g t h i s d i s t a n c e w i l l be decreased only about f o u r i n c h e s . Thus, u n l e s s t h e s t r u t i s s t r o k e d s i g n i f i c a n t l y t h e crewmen a r e r e q u i r e d t o s p r i n g up u s i n g t h e i r l e g s and arms t o b e s t advantage t o r e a c h t h e bottom rung of t h e l a d d e r from t h e footpad. �The second t a s k w i l l be t h e i n g r e s s o r t h e crewmen's movement through t h e h a t c h opening t o a s t a n d i n g p o s i t i o n i n s i d e t h e LM. The h a t c h opening and t h e space i n s i d e t h e LM a r e small. T h e r e f o r e , t h e crewmen must move slowly t o p r e v e n t p o s s i b l e damage t o t h e i r EMU'S o r t o t h e exposed LM equipment. Before t h e crew c l o s e s t h e h a t c h and b e g i n s t h e c a b i n r e p r e s s u r i z a t i o n , they w i l l j e t t i s o n t h e equipment they no l o n g e r need. The i t e m s t o j e t t i s o n a r e t h e used ECS c a n n i s t e r and b r a c k e t , OPS b r a c k e t s ( a d a p t e r s ) , and 3 a r m r e s t s . Numerous p i e c e s of l o o s e equipment w i l l b e l e f t on t h e l u n a r s u r f a c e a f t e r they have been deployed o r used d u r i n g t h e EVA. A complete l i s t of t h i s equipment except f o r a few pip-pins, b r a c k e t s , and o t h e r s m a l l p i e c e s of t h e l a r g e r p i e c e s of equipment l i s t e d , i s p r e s e n t e d a s Table 3-2 on t h e f o l l o w i n g page �TABLE 3-2 Loose Equipment L e f t on Lunar S u r f a c e During EVA . TV Equipment . . .. .. camera tripod h a n d l e l c a b l e assembly MESA b r a c k e t . S o l a r Wind Composition s t a f f Apollo Lunar Handtools scoop tongs e x t e n s i o n handle hammer gnomon Equipment stowed i n sample r e t u r n c o n t a i n e r s (outbound ) e x t r a York mesh packing m a t e r i a l SWC bag ( e x t r a ) spring scale unused s m a l l sample bags two c o r e tube b i t s two SRC s e a l p r o t e c t o r s environmental sample c o n t a i n e r s 0 r i n g s and s m a l l r o d s i n l i d s .. . .. . . . . .. - - . . . Apollo Lunar S u r f a c e Close-up Camera . EL Data Camera (magazine r e t u r n e d ) (film c a s s e t t e returned) EVA t e r m i n a t i o n Lunar Equipment Conveyor ECS c a n n i s t e r and b r a c k e t OPS b r a c k e t s Three a r m r e s t s Bag of used u r i n e bags . . . . . Post-EVA equipment j e t t i s o n Two P o r t a b l e L i f e Support Systems L e f t Hand S i d e Stowage Compartment (with equipment i n s i d e ) One a r m r e s t . . . �3.3 SUMMARY TIMELINE NOMINAL LUNAR SURFACE EVA n LEGEND I HCC.H ~YL:LRV." :: i.. I I ACIlVIIV ...'..., .. .~C.OV..l b0t~.0. 1.10 1:20 1439 \Irnt\<I it: is 1.40 *.:....z... .................................................... o u t COUY 5 m m . ru ~ m w t c r d o ~ p s s c c r ol.0 ~v OO(,YCITCO MCST/PMO~O IAYPLC :JUIC:,~S ius .Tact C L O I ~ . C DD . C I O I I < .OIDLO' L*' .Rat0 b C10SC.u. m .on* - .(a JcsLo."c:. 8.r ."CYWC I I ,.W.l"l*'S lOrYI [.,I> I 1XMIIVI.l am ! 0. T o o 1 C"M.l"I.lS 4- DO(.YI.113 ( A Y 4 1 C*L.L-"M .u~wt I);%* sw T O \ v 4 . ' v. ... c-*I .C,OSC S I P 6." I ~IILCCI < OWI OC.LO~YC.I .C.*.v 1.20 1.30 k ... $811 m s s * v c $cn\unr KC CL0SC.C. 1.10 I ..r I S ~ C t I P 1J 0 1 4 0 ' .OCPIO, I ur ~aeaa*~.. hi'\'\ -. --. -- -- 1:10.-. ��3.4 NOMINAL TIMELINE. LUNAR SURFACE EVA LMP - CD R - o+oo mm m a C r m ,m z m 0 mm z 00 D - oz x m - + I == C NOTE : DETAILED PROCEDURES ARE PRESENTED I N " F I N A L EVA PROCEDURES APOLLO 11" SUBMITTED BY EVA BRANCH, FC -zs 7JC <3 m - -I= W-I -I- TURN TV ON START SEQUENCE CAMERA (SC) I ' .I IPLAY UliT LEC I DESCEND TO FOOTPAD CHECK ASCENT PROCEDURES I z 3 r u I H O Z Z CHANGE SC FR TO 24/SEC STEP TO SURFACt RESTICHECK E14U I I I - .-ISTOW LEC - ~ - 0+10 - MONITOR CDR A C T I V I T Y PLAY OUT LEC MOVE TO'POSITION AND RELEASE MESA w cnD -m LMP - DEPRESS CABIN FROM 3.5 P S I OPEN HATCH INSURE SUBLIMATOR ICED PERFORM F I N A L SYSTEMS CHECKS CONFIRM "GO" FOR EVA - Wcn 0 CDR - II M O V E 1'HROUGH HATCH CHECK INGRFSS PROCEDURE I 11 1 APOLLO EDITION FINAL t 1 CHECK AND DISCUSS BALANCEISTABILITY I I 1 TO 121SEC VISUALLY MONIT~R CDR ACTIVITY PROVIDE CHECKLIST ASSISTANCE I + ASSIS CDR PLAY OUT LEC CHANGE SC F I L M MAG CHANGE FR TO 61SEC /-L MISSION CHANGE SC% - DATE JUNE 27, 1 9 6 9 rC/ I MISSION TIME I DAY1am I PAGE 1 �NOMINAL TIMELINE CDR - LMP - LMP - CDR - II I- REST/CHECK EMU CHECK LM AND EMU STA* sc 1 t UNSTOW CSC AllD DEPLOY HANDLE MONITOR AN; EXTEND BAG COLLECT SAMPLE + PHOTO EGRESS I DETACH BAG AND DISCARD HANDLE -I- I STOW SAMPLE I MONITOR TRANSFER STILL CAMERA TO SURFACE PREPARE FOR CAMERA TRANSFER ASSIST CDR PERFORM COMM CHECK AND PHOTO LMP C I REMOVE TRIPOD I PERF OR^ FI~AL LM AND EMU CHECK CONFIRM "GO" FOR EVA PLACE SPARE CAMERA ON LM FLOOR I MISSION APOLLO 1 1 I I FINAL I 1 JUNE t tI t DET'ERMI NE WALKING CAPABILITY REMOVE TV CABLE 1 I -I- REMOVE CAMERA CARRY TV TO DEPLOY S I T E L 1 EDITION f' \D LENS WA TO I t CHECK ERWIN AND LIGHTING STEP TO SURFACE REST/CHECK EMU + CHANGE FROM I CHECK AND REPORT LM STATUS DESCEND TO PAD CHECK ASCENT PROCEDURE C ECK BALANCE/STABILITY REACH CAPABILITY TETHER' CAMERA t I- I t PREPARE MESA FOR TV DEPLOYMENT REST/CHECK EMU MOVE TH'RU HATCH CHECK INGRESS PROCEDURE DATE 27. 1 9 6 9 MISSION TIME 112+54 - 113+18 I 1 DAY/ REV 5/20 I PAG€ 2 of 7 1 �NOMiNAL TIMELINE CDR - LMP - . II CDR - LMP - �NOMINAL TIMELINE LMP - CDR - ?' + CARRY ALSCC REPORT STATUS QUAD I V REPORT STATUS AND PHOTO -Y GEAR REMOVE PACKAGE 1 (PSE) PHOTO QUAD I V TAKE PHOTO PANORAMA + REMOVE PACKAGE 2 ( L R ~ ) I I PHOTO >Y GEAR 1 , PHOTO EASEP OFFLOAD TAKE CLOSE-UP PHOTOS TAKE CLOSE-UP PHOTOS QUAD. I11 + t 4- TRANSFER CAMERA TO CDR 1 OPEN SEQ BAY DOOR C I , PHOTO E A S E OFF LOAD MISSION APOLLO 11 I 1 EDITION FHVAL I 1 i t T RESTICHECK EMU C DEPLOY PSE $- DEPLOY L R ~ -IREPORT STATUS AND PHOTO QUAD I 1 t CLOSE SEQ BAY DOOR RESTISELECT DEPLOY S I T E CARRY CAMERAS TO CARRY EASEP DEPLOY S I T E PACKAGES REPORT POSITION TO DEPLOY S I T E FROM LM PHOTO -Z GEAR TETHER S T I L L CAMERA t T_L PHOTO qUAD I11 REPORT STATUS -Z GEAR 7' -1- REMOVE ALSCC FROM MESA AND DEPLOY 1 REPORT STATUS +Y GEAR 1 LMP - CDR - II I PHOTO L R ~ MOVE DATE JUNE 13, 1969 MISSION TIME 113+42 - 114+06 I % PSE T I 1 TAKE CLOSE-UP PHOTOS DAY/ REV 5/20 I PAGE 4 of 7 ��NOMINAL TIMELIN E CDR - LMP - CDR - LMP - T PLATFORM t RESTIPHOTO LMP 1 t REMOVE ALSCC F I L M STOW I N CSC POCKET STOW ALSCC F I L M I -L- t MOVE TO MESA PLACE SCOOP BY MESA MOVE TO MESA PLACE SAMPLE BAG ON SCALE t OPEN L A ~ G EENVIR. SAMPLE CONTAINER. COLLECT LOPSE MATERIAL -L + RETRIEVE SWC t HOLD CONTAINER SEAL AND STOW t SCOOP LOOSE + PACK SRC I F T I M E AVAILABLE COLLECT CORE SAMPLE CLOSE AND SEAL SRC MOVE TO LADDER CLEAN EMU t 1, APOLLO ASSIST CDR, + + HOLD S ~ CBAG 1. 11 1 T TRANSFER BULK SAMPLE SRC AND CAMERA MAG. MATERIAL INTO SAMPLE BAG PLACE SWC I N BAG MISSION CHANGE sc F I L M REORIENT CAMERA CHANGE FR TO 6/SEC I I PUSH STAFF INTO SURFACE. ASSESS FORCE PHOTO r REMOVE CAMERA MAGAZINE AND CONNECT TO LEC OPEN SMALL CONTAINER COLLECT ROCK SAMPLE HOLD CONTAINER SEAL AND STOW + INGRESS DISCONNECT AND STOW SRC AND CAMERA MAG. I I EDIVION. FINAL I DATE IJUNE 1 9 6~9 ~ , . MISSION TIME 114+30 - 114+54 1 DAY/ REV 5/20-21 I t PAW 6 of 7 I �NOMINAL TIMELINE CDR - LMP - - T - t1 -. JETTISON EQUIPMENT CLOSE HATCH - Ct STOP SC ' 2+40 LMP - CDR - CABIN REPRESS 1 - - DISCONNECT LEC AND - M I S S I O N TIME FINAL I JUNE 27, 1969 114+54 - 115+f8 I DAY/ REV 5/21 I PAaE 7 of 7 I �SUN I -z 100 FEET OF - FIGURE 3-9. - SCALE 0' PROBABLE AREAS FOR LUNAR SURFACE ACTIVITY 5' 10' �3.5 Detailed Procedures 3.5.1 Nominal Activities Sequence Section Event Final Pre-EVA Operations Page 40 CDR Initial EVA CDR Environmental Familarization Contingency Sample Collection Preliminary Checks LMP Initial EVA . VIII . VII TV Deployment LME' Environmental Familiarization SWC Deployment EVA and Environment Evaluation XI. Bulk Sample Collection LM Inspection* EASEP Deployment XIV . XV. XVI . XVII. * Documented Sample Collection LMP EVA Termination SRC Transfer CDR EVA Termination Nominally, the Apollo Lunar Surface Close-up . . Camera (ALSCC) will be deployed during the LM inspection. �3.5.2 Procedures LMP - CDR I. FINAL PRE-EVA OPEUTIONS NOTE: For t h e d e t a i l e d procedures of t h i s s e c t i o n , r e f e r t o t h e " F i n a l EVA Procedures Apollo ll", which is submitted by t h e EVA Branch, FCSD D e p r e s s u r i z e c a b i n from 3.5 p s i Open h a t c h I n s u r e s u b l i m a t o r iced Perform f i n a l systems checks Confirm "go" f o r EVA CDR INITIAL EVA 11. Move through h a t c h (with LEC t e t h e r e d ) Check i n g r e s s procedure A s s is t CDR ' . Perform communications . check w i t h MSFN - Compare l e v e l , c l a r i t y and r e l a y c a p a b i l i t y w i t h t h a t experienced i n s i d e t h e LM. NOTE: F u r t h e r mention of communications checks w i l l b e made only when communication c o n d i t i o n s change, however, t h e y w i l l b e conducted a s r e q u i r e d f o r system o r crewmen monitoring. Move t o p o s i t i o n on l a d d e r t o r e l e a s e MESA Play o u t LEC and u s e a s s a f e t y t e t h e r .. �CDR - Release MESA(1f MESA does n o t deploy, p u l l manual deployment lanyard l o c a t e d on l e f t s i d e of MESA) NOTE: I f t h e MESA w i l l n o t deploy a f t e r p u l l i n g t h e manual deployment lanyard, t h e following EVA t a s k s cannot b e accomplished: 1) 2) 3) 4) 5) 6) Turn TV on and v e r i f y TV reception . . . S t a r t sequence camera. Check o r i e n t a t i o n and frame r a t e a t 12 frameslsec TV Deployment (no TV coverage) SWC Deployment Bulk Sample C o l l e c t i o n Documented Sample C o l l e c t i o n SRC T r a n s f e r Close-up Photography Descend l a d d e r t o footpad. Checkpad-to-1adder.ascent procedures Play o u t LEC Change sequence camera (SC) frame r a t e (FR) t o 2 4 l s e c Step t o s u r f a c e R e s t b e s i d e ladderlcheck EMU. Check RCU. Report 02 and s u i t p r e s s u r e Change SC FR t o 12Isec. Check LM and EMU. Check RCU and r e p o r t 0 2 and s u i t p r e s s u r e Assess e g r e s s / i n g r e s s c a p a b i l i t y 111. CDR ENVIRONMENTAL FAMILIARIZATION Detach and temporarily stow LEC on gear s t r u t o r ladder I n t h e v i c i n i t y of t h e l a d d e r , check i n d i v i d u a l s t a b i l i t y and perform preliminary m o b i l i t y evaluation Check and r e p o r t b a l a n c e l s t a b i l i t y : a. b. c. - l e a n forward, E f f e c t of CG s h i f t backward, and t o each s i d e Downward reach A m motion e f f e c t s Visually monitor CDR a c t i v i t y . Provide c h e c k l i s t a s s is t a n c e �E v a l u a t e and r e p o r t walking capability: Change SC f i l m magazine when necessary. Change FR t o 61sec a. . B a l a n c e b. B e s t pace c. Boot p e n e t r a t i o n d. T r a c t i o n e. S o i l s c a t t e r i n g (cohesion) f . S o i l adhesion g. General comments . . . . . . ~ e s t l c h e c kEMU. Check RCU. Report 02 and s u i t p r e s s u r e . Report p h y s i c a l comfort. Assess EVA capsbility Check LM and EMU. Check RCU Report 02 and s u i t p r e s s u r e . . IV. . CONTINGENCY SAMPLE COLLECTION Remain w i t h i n a few f e e t of l a d d e r Remove t h e CSC from s u i t pocket Deploy t h e CSC h a n d l e and p u l l s t r a p a t b a s e of bag t o open C o l l e c t sample ( i n undisturbed area) P u l l l o c k i n g p i n on . h a n d l e r e l e a s e lever P r e s s r e l e a s e l e v e r and s e p a r a t e h a n d l e from l i p l b a g assembly Discard handle under o r away from LM Detach bag from l i p assembly Discard l i p assembly under o r away from LM S e a l sample bag Restow and s e c u r e bag i n s u i t pocket S t a r t SC. .Check FR a t 6 / s e c V i s u a l l y monitor CDR a c t i v i t y Reorient SC i f necessary �CDR - LMP V. PRELIMINARY CHECKS T r a n s f e r Hasselblad EL Data camera (with c o l o r f i l m and 60mm l e n s ) t o s u r f a c e : a. Remove LEC from temporary stowage l o c a t i o n Prepare t o t r a n s f e r t h e E l e c t r i c Hasselblad camera t o s u r f a c e b. Walk o u t +Z w i t h LEC P l a y o u t LEC. Remove LEC stowage bag and stow i n LHSSC c. T r a n s f e r camera t o s u r f a c e by p u l l i n g on lower s t r a p of LEC A s s i s t CDR, i f necessary d. Detach camera from LEC and t e t h e r t o s u i t . Mount camera on RCU b r a c k e t when d e s i r e d Change sequence camera FR t o llsec NOTE: Only t h e one Hasselblad camera is t r a n s f e r r e d t o t h e surface. I f a f a i l u r e o c c u r s , manual f i l m advancemand and a f u s e change a r e t h e only a c t i o n s p o s s i b l e t o c o r r e c t t h e malfunction. I f malfunction is not c o r r e c t e d , t h e 70mm Hasselblad, w i t h b l a c k and w h i t e f i l m and 80mm l e n s , can be transferred. e. P l a c e LEC back a t stowage location Check and r e p o r t LM s t a t u s . From immediate v i c i n i t y of t h e l a d d e r , check and r e p o r t : a. S t a b i l i t y of LM ( a l l pads contacting surface, t e r r a i n slope, boulders, c r a t e r s ) R e o r i e n t c'amera t o view CDR activity . (The LMP p r e p a r e s t o e g r e s s ) �CDR - b. Gear s t a t u s ( t a k e two photos, one each of +Y and -Y, and one of +Z p a d l s u r f a c e ) (1) Contact (2) P e n e t r a t i o n , s l i p , b u r i a l (3) S t r o k e . . (4) S o i l adhesion c . ? DPS s k i r t s t a t u s ( 1 photo) d. DPS e f f e c t on s u r f a c e : (1) Crater ' (2) R a d i a l e r o s i o n Perform f i n a l LM and EMU check. Confirm "GO" f o r two-man EVA P l a c e s p a r e Hasselblad camera on f l o o r a t 1 e f t . s i d e of +Z hatch. Check EVA t e t h e r attached (Refer t o t h e n e x t s e c t i o n f o r LMP e g r e s s p r o c e d u r e s ) . Check t e r r a i n s t a t u s f o r crew operations : . . a. Check s l o p e , o b s t r u c t i o n s and roughness i n (1) MESA a r e a (2) TV deployment a r e a (3) S-band antenna deployment area (4) Quad I a r e a b. Check l i g h t i n g l v i s i b i l i t y s t a t u s : (1) B r i g h t and d a r k a r e a s (2) TV deployment (3) MESA (4) S-band antenna a r e a (5) General sampling a r e a s ( t a k e two ( s t e r e o ) photos of b u l k sample and one photo, c l o s e up, of contingency sample a r e a ) (6) Up sun (7) Cross sun (two photos, one each d i r e c t i o n ) (8) Down sun LMP INITIAL EVA Res t/Monitor and photograph LMP e g r e s s and d e s c e n t t o R e o r i e n t SC . . . surface Photo (3) LMP Move through hatch. Check i n g r e s s procedure ( P u l l +Z hatch closed) �CDR - LMP Perform communications check (Include r e l a y check with CSM, i f p o s s i b l e ) Photo (3) LMP Descend l a d d e r t o footpad Check pad-to-ladder procedures Photo (3) LMP ascent Step t o s u r f a c e (Deploy TV, see procedures below) Rest b e s i d e ladderlcheck Assess e g r e s s l i n g r e s s capabilities EMU. VII. TV DEPLOYMENT Walk t o MESA Adjust MESA h e i g h t , i f necessary, by p u l l i n g upward on adjustment strap P u l l s t r a p (velcroed) t o remove MESA thermal b l a n k e t from around TV l e n s Complete removal of thermal blanket Remove t r i p o d from MESA: a. P u l l two s t r a p s t o unsnap b. c. d. e. tripod L i f t t r i p o d from MESA Extend t e l e s c o p i n g s e c t i o n Deploy l e g s P l a c e on s u r f a c e near r i g h t s i d e of MESA Walk t o r i g h t s i d e of MESA Remove wide angle l e n s from TV camera and stow on MESA holder Remove LD l e n s from holder and a t t a c h t o camera P u l l s e v e r a l f e e t of TV cable from MESA . (After completion of a r e s t period t h e LMP conducts environmental f a m i l i a r i z a t i o n , see S e c t i o n VIII) �CDR Remove camera from MESA: a. Pull the two pins at the forward edge of mounting frame b. Grasp TV handle and rotate TV toward rear of MESA to free from frame c. Lift camera from frame d. Check camera temperature and report (cold, normal, hot) Place camera on tripod. camera secure Check Carry camera with tripod to site to view subsequent EVA operations (See figure 3-4) Take a step-wise, fast-scan (10 frameslsec) panorama or, if time not available, select several points of interest. Do not point camera within 20" to sun. Start panorama at approximates 22" from an upsun view, move through down sun, continue to other view 22" from up sun. Place camera on surface for a few seconds at approximately 22 112" increments. (15 increments are required for the panorama) Recheck camera temp. and report. Place TV on surface for optimum coverage of surface activity (See Figure 3-4) Move near LMP. Restlcheck EMU. Check RCU. Report 02 and suit pressure. Photo SWC (stereo pair) after LMP deploys it. Return to MESA As required, pull more TV cable from MESA �LMP - CDR - VIII. LMP ENVIRONMENTAL FAMILIARIZATION (At t h i s p o i n t t h e CDR i s deploying t h e TV, s e e S e c t i o n VII) I n t h e v i c i n i t y of. l a d d e r and i n view of TV (and sequence camera, i f pract i c a l ) , check and r e p o r t balance/s t a b i l i t y : a. E f f e c t of CG s h i f t - l e a n forward, backward, and t o each s i d e b. Downward r e a c h c. A r m motion e f f e c t s E v a l u a t e and r e p o r t r e a c h c a p a b i l i t y (with and without support): a . Right up b Right down c. Both up and down . NOTE: Perform f o l l o w i n g e v a l u a t i o n s w i t h i n a few yards of SIC and i n view of sequence camera, i f practical E v a l u a t e and r e p o r t walking capability: a. b. c. d. Pace Stability Traction General e v a l u a t i o n ~ e s t / c h e c kEMU. Check RCU. Report oxygen and s u i t p r e s s u r e . Report p h y s i c a l comfort. Assess EVA capability �CDR - LMF' SWC DEPLOYMENT (At t h i s time t h e CDR is dep l o y i n g t h e TV, s e e S e c t i o n VII) a E r e c t SRC t a b l e : . . a. P u l l Velcro t a b s t o free table b. P u l l t a b l e forward from stowed p o s i t i o n and r o t a t e i n t o horizontal position c. Attach Velcro t a p e t o hold t a b l e i n correct position ( l e v e l , f o r e and a f t ) P u l l t h e two s t r a p s h o l d i n g SWC and remove SWC from MESA Walk t o s u n l i t a r e a Deploy SWC: a. Extend each s e c t i o n of s t a f f u n t i l i t l o c k s . ( r e d band should b e v i s i b l e ) Apply a compressing f o r c e t o each s e c t i o n t o check s e c t i o n s locked b. Extend shade c y l i n d e r and r o t a t e toward r e d s i d e of p i v o t p o i n t , i.e., r e d t o red c. Extend f o i l shade and hook t o lower p o r t i o n of s t a f f d. P r e s s s t a f f i n t o surf a c e w i t h f o i l normal t o sun ( s i d e marked SUN t o Sun) �CDR - LMP X. EVA AND ENVIRONMENT EVALUATION Remove camera from MESA and t e t h e r when r e q u i r e d i n t h e following evaluation NOTE: The f o l l o w i n g l i s t of t a s k s i s p r e s e n t e d a s a guide. The a c t i v i t i e s w i t h i n t h i s p e r i o d are n o t l i m i t e d t o t h e items l i s t e d o r t h e o r d e r i n which they appear. I f necessary f u r t h e r e v a l u a t e: a. E f f e c t of CG s h i f t b (leaning, reach, e t c . Walking capability .) I n u n d i s t u r b e d a r e a and i n view of TV a n d . SC, i f p r a c t i c a l , observe and report : a. Best pace b. Technique f o r s t a r t i n g and s t o p p i n g c. Balance a t i n c r e a s e d pace and l e n g t h of s t e p d. T r a c t i o n e. Dust f . Boot p e n e t r a t i o n ( t a k e stereo pair) g. S c u f f i n g h. Cohesion i. Adhesion (photo boots) 3 . General e v a l u a t i o n of EVA capability �CDR - I n each d i r e c t i o n , up sun, down sun and c r o s s sun, observe and r e p o r t s u r f a c e : a. b. c. d. e. f. Brightness/reflections Color p e r c e p t i o n Contrast v a r i a t i o n Texture determination R e f l e c t i o n i n shadow Rock and c r a t e r distribution g. General t e r r a i n evaluation h. Visual and t e r r a i n phenomena d i f f e r e n t from t h a t expected Check EMU s t a t u s w i t h MSFN af t e r stay i n sunlight. Report comfort /problems Move t o shadow edge and repeat l i g h t i n g / v i s i b i l i t y and t e r r a i n e v a l u a t i o n a s above. A d d i t i o n a l l y , observe shadow edge sharpness (look down sun) Check EMU s t a t u s w i t h MSFN a f t e r stay. Take 12 photo panorama (from p o s i t i o n 20 f e e t i n f r o n t of +Z pad). A s panorama is taken, e s t i m a t e d i s tance t o s e v e r a l prominent terrrain features. Repeat e v a l u a t i o n , a s above, i n shadow Check EMU af t e r s t a y i n shadow �CDR - LMP XI. BULK SAMPLE COLLECTION (The LMP i s conducting t h e EVA and Environment E v a l u a t i o n , S e c t i o n X) Remove camera and p l a c e on MESA P r e p a r e MESA: a. Proceed t o MESA b. I n s u r e a r e a about MESA is s u i t a b l e f o r operations c. Adjust h e i g h t of MESA, i f required d. I n s u r e a l l equipment i s accessible Deploy ETB: a. Unfold and p o s i t i o n bag on r i g h t s i d e of MESA (Check bag t o p f o l d e d i n s i d e bag) . P r e p a r e SRC and ALHT: a. Unstow scoop and hammer. P l a c e i n ETB b. Check s e c u r i t y of SRC t a b l e c. Release b u l k sample SRC c a r r y h a n d l e from d e t e n t p o s i t i o n d. R o t a t e h a n d l e 90' clockwise t o r e l e a s e SRC from MESA e. P u l l p e r p e n d i c u l a r t o MESA t o p w i t h c a r r y handle t o remove from stowage p o s i t i o n f . P l a c e SRC on t a b l e w i t h T-handle up and SRC a l i g n e d with t h e t a b l e g. R o t a t e and p l a c e t h e SRC on t a b l e w i t h SRC h a n d l e pointing away from t h e s p a c e c r a f t h. Release t h e two s t r a p l a t c h e s by p r e s s i n g t h e l a t c h l o c k i n g mechanism, w i t h t h e hand on t h e r e l e a s e handle, i n a sideways motion toward t h e c e n t e r of t h e SRC and r o t a t i n g t h e handle forward and upward . �i. Continuing t o grasp second . s t r a p l a t c h r e l e a s e handle, a f t e r relase, rotate the SRC top to' a n open s t a b l e ' p o s i t i o n . NOTE: I f necessary r e s t r a i n SRC with o t h e r hand on c a r r y handle i n order t o break seal j. Check t h e seal s p a c e r is s t i l l i n p l a c e over t h e s e a l k. Unpack SRC. P l a c e packing m a t e r i a l , and s m a l l sample bags i n SRC l i d , i n t r a n s f e r bag o r on MESA 1.. Remove s p r i n g s c a l e m. Hook s c a l e t o l e f t f r o n t of MESA n. Attach l a r g e sample bag t o s c a l e o. P l a c e SWC stowage bag i n SRC l i d o r on MESA NOTE: I f p r a c t i c a l c o l l e c t samples i n view of TV and sequence camera (NOTE: I f p r a c t i c a l use t h e scoop t o c o l l e c t rocks and loose m a t e r i a l simultaneously. Attempt t o c o l l e c t same volume of rocks a s loose m a t e r i a l ) C o l l e c t rock fragments: a. P u l l s t r a p t o f r e e v i b r a t i o n a t t e n u a t o r from tongs b. Remove t h e tongs from t h e MESA, p u l l t h e two lanyards t o r e l e a s e snaps c. Move w i t h i n s e v e r a l yards of t h e MESA t o c o l l e c t rock fragments placing each fragment i n t o t h e sample bag a t t h e t i m e of collection d. A t t h e completion of fragment sampling, place t h e tongs i n temporary stowage i n t h e MESA o r ETB �CDR R e s t l c h e c k EMU systems Collect loose material: a. Remove e x t e n s i o n h a n d l e from stowed p o s i t i o n on MESA. P u l l two snap l a n y a r d s on e x t e n s i o n h a n d l e t o r e l e a s e . Remove v i b r a t i o n a t t e n u a t o r from s m a l l handle. b. Remove scoop from ETB and connect t o e x t e n s i o n handle c . U s e scoop t o f i l l sample bag w i t h l o o s e m a t e r i a l . Comment on c o l l e c t i o n p r o c e s s , s o i l adhesion and cohesion, d i f f i c u l t y of ..scooping, volume of m a t e r i a l , general evaluation . d. Disconnect e x t e n s i o n handle . from scoop. P l a c e scoop 'and e x t e n s i o n h a n d l e i n temporary stowage on MESA o r i n ETB Res t l c h e c k EMU systems Pack and s e a l SRC: a. Remove sample bag from s p r i n g scale b. P l a c e sample bag i n SRC c. Close bag and p l a c e bag i n c e n t e r of SRC s o t h a t bag ends a r e toward SRC ends. d. P l a c e packing m a t e r i a l i n SRC t o minimize v o i d space U s e c a u t i o n t o keep SRC s e a l clean. e. Remove s e a l p r o t e c t o r . If a n O-ring s e a l is l o o s e , remove from SRC and d i s c a r d �CDR - LMP - f . Rotate t h e top closed with a s t r a p l a t c h handle g. S e a l t h e SRC by r o t a t i n g t h e two s t r a p l a t c h e s downward t o t h e locked p o s i t i o n ' P r e p a r e f o r SRC t r a n s f e r : a. R e t r i e v e LEC from stowed position b. Walk t o SRC c. A t t a c h LEC lower hook (marked w i t h "L") t o SRC t o p - l e f t f r o n t bracket d. Attach LEC upper hook (marked w i t h "R") t o t h e SRC t o p - r i g h t r e a r b r a c k e t and l o c k hook R e s t l c h e c k EMU XII. (At t h i s ' p o i n t t h e CDR i s comp l e t i n g t h e Bulk Sample Collect i o n , S e c t i o n XI) LM INSPECTION During i n s p e c t i o n e v a l u a t e v i s u a l perception Report s t a t u s of Quad I: a. Both LM s t a g e s (1) Coating (2) Dust (3) S h i e l d i n g b. Ascent s t a g e (one photo) (1) RCS (2) Rendezvous r a d a r c. Descent s t a g e (one photo) (1) Engine s k i r t , Report s t a t u s of +Z gear: a. Main s t r u t ( t a k e one photo) b. Secondary s t r u t s (two photos, one on each side) c. Take s t e r e o p a i r of padlsurf ace �Photo a r e a where b u l k sample was c o l l e c t e d Deploy ALSCC : (Deployment of t h e ALSCC w i l l b e delayed u n t i l t h e documented sample c o l l e c t i o n i f behind i n the timeline) . a. Remove i s o l a t o r l a t c h p i n and p i v o t cover b. P u l l camera from MESA c. P l a c e camera on secondary g e a r s t r u t and e x e r t . p r e s s u r e on camera cover. P u l l t h e two s k i r t l a n y a r d s d. R o t a t e handle r e t a i n i n g latch e. Swing handle clockwise 150° and p u l l u n t i l f u l l y extended f . P l a c e camera on s u r f a c e ALSCC OPERATION Close-up photographs w i l l b e t a k e n by e i t h e r crewman when time i s a v a i l a b l e between or during other tasks. Several times w i t h i n t h e EVA a r e sugg e s t e d when i t may b e convenient f o r t h e crew t o t a k e photos. T h i s i s n o t a requirement t o t a k e photos nor does i t p r o h i b i t . them from o b t a i n i n g photographs a t o t h e r times which may b e feasible. I n g e n e r a l t h e camera o p e r a t i o n is : a. Estimate p o s i t i o n of o b j e c t p l a n e r e l a t i v e t o camera bearing surface b. P o s i t i o n camera over o b j e c t (Describe o b j e c t and l o c a t i o n ) , �CDR - c. I f o b j e c t is below ALSCC bearing surface depress s k i r t u n t i l o b j e c t i s w i t h i n focus plane d. I f o b j e c t is above b e a r i n g s u r f a c e t i l t camera back u n t i l o b j e c t i s w i t h i n focus p l a n e e. A c t i v a t e t r i g g e r l o c a t e d on handle g r i p f . Read and r e p o r t frame c o u n t e r g. Observe c y c l e completion by l i g h t on handle Carry t h e ALSCC around t h e LM d u r i n g t h e i n s p e c t i o n and t a k e photos a s p r a c t i c a l Report s t a t u s of Quad IV: a. Both LM s t a g e s (1) Coating (2) Dust (3) S h i e l d i n g b. Ascent s t a g e (1) RCS (2) St e e r a b l e antenna (3) Rendezvous r a d a r c. Descent s t a g e (1) Descent engine s k i r t (2) MESA Report s t a t u s of +Y g e a r assembly: a. Main s t r u t b. Secondary s t r u t s . Take one photo of A/S Take one photo of s k i r t Take one photo of MESA ( I n c l u d e a l l Quad I V , i f practical) Take one photo of main s t r u t Take two photos, one on each s i d e of secondary s t r u t s Take s t e r e o p a i r of pad/ surface �CDR R e s t l e v a l u a t e and r e p o r t l i g h t i n g / v i s i b i l i t y i n a l l directions, p a r t i c u l a r l y SIC r e f l e c t i o n s . Observe and r e p o r t t e r r a i n c h a r a c t e r i s t i c s . Estimate dist a n c e t o s e v e r a l prominent t e r r a i n f e a t u r e s . Take close-up photos i f p o s s i b l e - .LMP Take panorama (12 photos) from p o s i t i o n approx 20 f t o u t from +Y pad and 30 deg CW from +Y a x i s o r 120 deg from l a s t panorama Report s t a t u s of Quad 111: a. Both LM s t a g e s (same a s Quad IV) b. Ascent s t a g e (1) RCS (2) St e e r a b l e antenna (3) VHF antenna c. Descent s t a g e (1) P r o p e l l a n t v e n t s (2) F u e l v e n t (3) Tanks (Oxygen, Helium (2)) (4) Descent engine s k i r t (5) Note i f s u r f a c e d i s c o l o r e d Report s t a t u s of -Z g e a r assembly (same items a s +Y and: Take one photo of A/S , Take one photo of s k i r t (Photo i f s u r f a c e d i s c o l o r e d ) Take same photos a s +Y a. Landing t r a c k b. O x i d i z e r v e n t c EVA antenna) . . Receive camera and t e t h e r t o s u i t Hand Hasselb l a d camera t o CDR Report s t a t u s of Quad 11: (The LMP b e g i n s t h e . EASEP deployment. See t h e following s e c t i o n ) a. Both IN s t a g e s (same a s Quad IV) b. Descent s t a g e (one photo) (1) Landing r a d a r (2) SEQ bay ' T a k e 12 photo panorama (from 20 f t o u t from -Y pad and 30' CCW from -Y a x i s o r 120' from l a s t panorama position) �CDR - LMP Report s t a t u s of -Y g e a r assembly: a. Main s t r u t ( t a k e one photo) b. Secondary s t r u t s (one photo from each s i d e ) c. P a d l s u r f a c e ( t a k e s t e r e o pair) XIII. (At t h i s p o i n t t h e CDR i s completing t h e LM i n s p e c t i o n . See t h e precedi.ng s e c t i o n ) NOTE: I f LMP cannot r a i s e door, s t a n d c l e a r of d o o r , a n d manually' a s s i s t ' EASEP DEPLOYMENT Open SEQ bay door: a. Remove thermal cover from door lanyard b. R e t r i e v e l a n y a r d from r i g h t s i d e of SEQ bay (remove lower v e l c r o strap) c. Move t o p o s i t i o n c l e a r of door d. p u l l w h i t e of lanyard t o r a i s e door e. Temporarily stow lanyard on s t r u t f . I f Quad I1 is i n a low a t t i t u d e connect f o l d e d doors w i t h v e l c r o s t r a p PACKAGES REMOVED BY BOOMS Photograph package removal Remove Package 1 (PSE): a. R e t r i v e boom l a n y a r d from package, (handle) . ' . b. Move t o p o s i t o n c l e a r of package (approximately . . 10 f e e t ) c. P u l l w h i t e p o r t i o n of lanyard t o unlock and move package from SEQ bay t o f u l l y extended boom position �CDR - LMP d. P u l l b l a c k and w h i t e s t r i p e d p o r t i o n of lanyard t o lower package t o s u r f a c e e. R e l e a s e w h i t e p o r t i o n of lanyard from b a s e of package f . P u l l s m a l l lanyard ( v e l c r o e d t o handle) on package t o r e l e a s e boom c a b l e and l a n y a r d s . Reattach lanyard t o v e l c r o g. Move package c l e a r h. P u l l b l a c k and w h i t e s t r i p e d lanyard t o r e t r a c t boom ( o r push boom back w i t h hand) Remove Package 2 (LR') : a. Repeat Package 1 procedure ( s e t package c l e a r of SEQ bay MANUAL PACKAGE REMOVAL Remove Package 1: . a. P u l l s m a l l l a n y a r d , a t t o p o r bottom of package, t o r e l e a s e hockey s t i c k from boom b. Remove deployment l a n y a r d from package and p u l l w h i t e p o r t i o n t o unlock package from bay c. Release w h i t e p o r t i o n of lanyard from b a s e of package d. Move deployment l a n y a r d t o s i d e c l e a r of package e. Manually p u l l package c l e a r of SEQ bay f . S e t package on s u r f a c e c l e a r of bay a r e a �LMP - CDR - Remove Package 2: a. Repeat Package 1 procedure NOTE: Simultaneous accomplishment, although i n d i c a t e d of t h e following tasks, is not required. Photo LMP and t a k e close-up photos a s p r a c t i c a l Close SEQ bay door: a. R e t r i e v e door l a n y a r d b. Move t o p o s i t i o n c l e a r of door c. P u l l b l a c k and w h i t e s t r i p e p o r t i o n of l a n y a r d u n t i l door is c l o s e d d. Discard l a n y a r d . 3 S e l e c t s i t e f o r PSE and LR deployments, nominally 70 f t s o u t h of t h e SIC . Move to'deployment s i t e w i t h cameras. E s t i m a t e d i s t a n c e and p o s i t i o n w i t h r e s p e c t t o t h e LM P l a c e LR3 w i t h b a s e toward Earth. (Astronaut f a c e s e a s t f o r S i t e s 1 and 2 and west f o r S i t e s 3,4, and 5). R e s t / prepare a r e a ( c l e a r rocks, smooth s u r f a c e as r e q u i r e d ) 3 Carry PSE and LR t o deployment s i t e (Nominally 70 f e e t out t h e LM-Y a x i s . Report s i t e 10cat i o n i f i t is n o t nominal) 3 P l a c e LR package on s u r f a c e (on end) i n a c l e a r , l e v e l l o c a t i o n , i f p r a c t i c a l . Move PSE approximately 1 0 f e e t f u r t h e r from T.,M and p l a c e on s u r f a c e w i t h b a s e toward n o r t h (Arrow on handle p o i n t s t o south) 3 Deploy LR : a. Simultaneously g r a s p deployment boom ("hockey s t i c k " ) and p u l l p i n ' i n s i d e c a r r y handle. Remove and d i s c a r h "hockey s t i c k " a* Res t / c h e c k EMU �CDR b . ment Simultaneously g r a s p deployh a n d l e and r e l e a s e r i n g c. d. e. f. . * ( L e f t s i d e of package) t o release deployment handle p u l l pin O P u l l deployment handle t o extend handle s i x inches, t o the f i r s t d e t e n t p o s i t i o n , and t o p a r t i a l l y r e l e a s e a r r a y . Discard handle release ring Grasp p u l l r i n g on a r r a y t i l t i n g handle, p u l l t o remove p r o t e c t i v e cover. Discard cover @ Grasp deployment handle t o s t e a d y package. @ Grasp a r r a y t i l t i n g handle, push down r o t a t e handle 45'. P u l l outward t o extend t o d e t e n t p o s i t i o n (9.5 i n c h e s ) and complete a r r a y r e l e a s e @ Use deployment handle t o s t e a d y package. Use a r r a y t i l t i n g handle t o t i l t a r r a y ( t o d e t e n t f o r landing s i t e ) Deploy PSE: a. P r e p a r e a r e a (move r o c k s , . etc.) i f required b. From b a s e of package p u l l l a n y a r d t o r e l e a s e gnomon @ c. Grasp c a r r y h a n d l e w i t h one hand and u s e t h e o t h e r t o remove and d i s c a r d t h e r i g h t s o l a r panel-restraini n g p u l l p i n @ and p a n e l support bracket p u l l p i n @ d. Grasp f i r s t s o l a r p a n e l support bracket, r o t a t e b r a c k e t forward l i f t b r a c k e t upward t o r e l e a s e and remove f i r s t r e a r support bracket-p u l l pin. @ Discard b r a c k e t / l a n y a r d / p u l l p i n The c i r c l e d numbers and symbols correspond t o d e c a l s on t h e packages. g. R e l e a s e t i l t i n g handle (should s p r i n g back i n t o stowed position) h. Depress t r i g g e r on deployment handle, p u l l handle t o extend t o f u l l @ e x t e n t (an a d d i t i o n a l 27 inches) and r o t a t e package t o lunar surface i. Check and r e p o r t experiment a l i g n e d and l e v e l t o w i t h i n Use gnomon +5O. - @1-1 shadow c a s t on p a r t i a l compass r o s e f o r alignment. Use bubble f o r l e v e l i n d i c a t i o n . Use deployment h a n d l e t o a l i g n and l e v e l as r e q u i r e d e. Repeat procedures c. and d. f o r t h e l e f t s o l a r panel bracket @ @ @ f . From s i d e of PSE p u l l deployment h a n d l e ("worki n g height") p i p p i n @ and remove "hockey s t i c k " @ g. Grasp deployment h a n d l e , r o t a t e and p u l l t o extend t o 30 i n c h working h e i g h t and l o c k i n p l a c e @ h. Use deployment handle t o r o t a t e package t o s u r f a c e i. With deployment h a n d l e , embed package mounting t a b s i n l u n a r s u r f a c e (smooth s u r f a c e and a l i g n package) 0 ~nm-1 �CDR - Photograph s c i e n t i f i c packages: CAUTION : Do n o t walk up-sun of t h e PSE. Shadows on t h e s o l a r p a n e l s affect internal electronics a. Take c l o s e u p photo of LR3 b. Take s t e r e o p a i r of LR3 c. Take one photo from about same distance a s stereo p a i r but a t e n t i r e l y d i f f e r e n t angle d.. Move t o PSE e. Repeat photos as i n a , b , and c j. Check and r e p o r t experiment a l i g n e d and l e v e l t o withi n i-5' a s i n d i c a t e d by gnoKon shadow c a s t on part i a l compass r o s e and bubble l e v e l , r e s p e c t i v e l y . Use deployment h a n d l e t o a l i g n and l e v e l as r e q u i r e d . k. P u l l antenna r e l e a s e lanyard from deployment handle ( v e l c r o e d t o handle) 1. P u l l l a n y a r d t o deploy s o l a r p a n e l s and antenna NOTE: . I f p a n e l s do n o t deploy, s t a n d c l e a r of deployment a r e a and check r e a r s u p p o r t b r a c k e t s c l e a r of s o l a r p a n e l s and r e l e a s e l e v e r s (underneath forward edge of p a n e l s ) p u l l e d m. R o t a t e antenna t o designated landin o f f s e t ( s i t e dependent) n. Recheck package l e v e l and a l i g n e d . Report shadow on compass r o s e &) Move t o t h e Quad IV a r e a Move t o MESA w i t h ALSCC.: Take photos a s p r a c t i c a l . Photo f o o t p r i n t made w h i l e c a r r y i n g EASEP R e s t l c h e c k EMU Restlcheck EMU XIV. ~ e s t / p h o t oLMP. close-up photos Take ' - DOCUMENTED SAMPLE COLLECTION T r a n s f e r b u l k sample SRC t o footpad o r g e a r s t r u t s : . . a. Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t .b. L i f t SRC from t a b l e by l e f t (lower) hook @ �CDR c. Carry SRC and p l a c e on footpad o r secondary struts d. Temporarily stow LEC on gear s t r u t e. Return t o MESA P r e p a r e documented sample SRC f o r sample c o l l e c t i o n : a. Check s e c u r i t y of t a b l e b. P u l l t h e lanyard on l e f t s i d e of TV mounting b r a c k e t t o r e l e a s e t h e two p u l l pins. c. Remove and d i s c a r d b r a c k e t under LM d. Release DS SRC c a r r y h a n d l e from d e t e n t p o s i t i o n e. R o t a t e handle 90' clockwise t o r e l e a s e SRC from MESA f . P u l l perpendicular t o MESA top w i t h c a r r y h a n d l e t o remove from stowage position g. P l a c e SRC on t a b l e w i t h T-handle up and SRC a l i g n e d with the t a b l e h. R o t a t e and p l a c e . t h e SRC on t a b l e w i t h SRC handle p o i n t i n g away from t h e spacecraft i. Release t h e two s t r a p l a t c h e s by p r e s s i n g t h e l a t c h l o c k i n g mechanism w i t h t h e hand on t h e r e l e a s e handle i n a sideways motion toward t h e c e n t e r of t h e SRC and r o t a t i n g t h e handle forward and upward �CDR j. Continuing t o g r a s p second strap latch release handle, a f t e r r e l e a s e , r o t a t e t h e SRC t o p t o an open s t a b l e p o s i t i o n . NOTE: I f necessary res t r a i n SRC w i t h o t h e r hand on c a r r y h a n d l e i n o r d e r t o break s e a l k. Check t h e s e a l s p a c e r i s s t i l l i n p l a c e over t h e bottom s e a l 1. Remove and stow packing m a t e r i a l on SRC l i d , o r i n MESA o r ETB Remove one c o r e t u b e from SRC and p l a c e i n SRC l i d o r ETB . n. Remove t u b e caps and p l a c e i n SRC l i d (two caps . . . wrapped i n packing m a t e r i a l ) 0. Remove small sample bag c o n t a i n i n g York mesh. S e a l bag and p l a c e i n SRC l i d Walk t o LMP ', C o l l e c t c o r e t u b e sample: Take s t e r e o p a i r a f t e r t u b e i s pushed i n t o s u r f a c e ' a. Remove c o r e t u b e from SRC (check b i t a t t a c h e d ) and connect t o t h e e x t e n s i o n handle b. Remove hammer from ETB c. Move t o an u n d i s t u r b e d p o i n t n e a r t h e MESA ( i n view of TV, i f p r a c t i c a l ) d. P l a c e t h e c o r e t u b e a t t h e sampling l o c a t i o n . Push tube i n t o surface t h e l e n g t h of t h e tube. Drive w i t h t h e hammer i f n e c e s s a r y e. R e t r i e v e t u b e by p u l l i n g a l o n g its vertical axis, rotating i f necessary �CDR - I f procedure above i s n o t p r a c t i c a l o r i f t i m e perm i t s , p l a c e gnomon n e a r p r o s p e c t i v e fragment and/or s o i l sample ( n e a r s e v e r a l samples i f p o s s i b l e ) and t a k e two photos of sample s i t e . From approximately f i v e f e e t away, t a k e two photos ( s t e r e o p a i r ) from n e a r 90' t o sun l i n e NOTE: The types of samples and t h e o r d e r i n which they a r e coll e c t e d w i l l b e dependent on t h e t e r r a i n features investigated and crew judgement on t h e b e s t i n v e s t i g a t i v e approach w i t h i n operational limitations. . . Remove a s m a l l b a g ( s ) from l a r g e bag. Report number on bag. (Bags a r e numbered 1 through 14) Open s m a l l bag and hold f o r LMP S e a l small bag and p l a c e i n i n l a r g e c o l l e c t i o n bag Photograph a r e a ( s ) where sample(s) was taken C o l l e c t sample(s) w i t h scoop o r tongs. P l a c e i n bag ( c o l l e c t s e v e r a l samples i f possible) NOTE: The scoop can be used t o simultaneously.collect a small fragment and a s m a l l q u a n t i t y of l o o s e m a t e r i a l S e l e c t a n o t h e r sample and d e s c r i b e o r s e l e c t a new sample a r e a Pick up gnomon ( i f gnomon cannot be conveniently included i n photographs of n e x t sample) �CDR - I f procedure above i s n o t p r a c t i c a l o r i f t i m e perm i t s , p l a c e gnomon n e a r p r o s p e c t i v e fragment and/or s o i l sample ( n e a r s e v e r a l samples i f p o s s i b l e ) and t a k e two photos of sample s i t e . From approximately f i v e f e e t away, t a k e two photos ( s t e r e o p a i r ) from n e a r 90' t o sun l i n e NOTE: The types of samples and t h e o r d e r i n which they a r e coll e c t e d w i l l be dependent on t h e t e r r a i n features investigated and crew judgement on t h e b e s t i n v e s t i g a t i v e approach w i t h i n operational limitations. . . Remove a s m a l l bag(s) from l a r g e bag. Report number on bag. (Bags a r e numbered 1 through 14) Open s m a l l bag and hold f o r LMP S e a l s m a l l bag and p l a c e i n i n l a r g e c o l l e c t i o n bag Photograph a r e a ( s ) where sample(s) was taken C o l l e c t sample(s) w i t h scoop o r tongs. P l a c e i n bag ( c o l l e c t s e v e r a l samples i f possible) NOTE: The scoop can be used t o simultaneously.collect a small fragment and a s m a l l q u a n t i t y of l o o s e m a t e r i a l S e l e c t a n o t h e r sample and d e s c r i b e o r s e l e c t a new sample a r e a Pick up gnomon ( i f gnomon cannot be conveniently included i n photographs of next sample) �CDR Move t o a new sampling a r e a Repeat sampling procedure a t new s i t e ( s ) - u n t i l t h e c o l l e c t i o n bag is f i l l e d o r t h e a l l o t t e d time h a s elapsed. ~ e s t l c h e c kEMU as a p p r o p r i a t e . Take s u r f a c e close-up photographs i f feasible Move t o MESA w i t h s t i l l and close-up cameras Move t o MESA w i t h tongs, scoop, and samples Remove ALSCC f i l m c a s s e t t e and stow: a . P u l l t h e two cover l a n y a r d s and remove cover b. R o t a t e c a s s e t t e f i l m cutter lever c. L i f t c a s s e t t e r e t a i n i n g arm d. Remove c a s s e t t e a n d . p l a c e i n CSC pocket on CDR's s u i t . Close CSC pocket Remove l a r g e sample bag from LMP and a t t a c h t o s p r i n g s c a l e on MESA P l a c e scoop by o r on MESA Hold c o n t a i n e r f o r LMP Hand c o n t a i n e r t o CDR Remove sample of t h e i n the Remove t h e environmental container, the l a r g e r two s m a l l c o n t a i n e r s SRC, and open. o-ring from s e a l �CDR Use scoop to collect loose material from an undisturbed area where bulk sample was taken. Place sample in container. Place scoop by MESA Seal container and place in SRC Remove the gas analysis container from SRC and open. Remove o-ring seal Hand container to CDR Hold container for LMP Use tongs to collect a small rock fragment from bulk sample area and place in container. Seal container and place in SRC Detach tongs and place in ETB Recover SWC: Use scoop to collect rocks and loose material. Fill large sample bag to designated weight or volume Move to SWC Withdraw staff from surface Roll up foil Rotate foil roller to detach position and remove from staff Let staff rest on surface, vertically and with only its weight acting on surface, report depth of penetration Push staff into surface as deep as possible Assess amount of force applied and staff depth If time permits photograph staff and repeat e and f several times. Check staff rigidity in surface Carry SWC foil to MESA Place bag in SRC. Seal bag Remove SWC bag from temporary stowage on MESA and open Hold bag for CDR Insert foil into bag Seal SWC bag and place in SRC Collect second core tube sample if time available (See procedures on page 55) If time not available assist CDR Place York mesh sample (in SRC lid) in SRC. Place packing material in SRC to minimize void space 68 �CDR - T r a n s f e r b u l k sample SRC and magazine: ( I f t h e r e i s time f o r t h e t r a n s f e r of only one SRC, t h e b u l k sample SRC w i l l be t r a n s f e r r e d ) a . Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t b. Grasp loop g r i p on t h e LEC top l i n e c. L i f t SRC from s t r u t d. Walk t o t h e f r o n t of t h e . l a d d e r w i t h SRC suspended on LEC e. Walk away from l a d d e r ( i n +Z d i r e c t i o n ) w h i l e h o l d i n g LEC t o p . s t r a p (loop) t o t r a n s f e r magaz i n e and SRC t o A/S Assist CDR, i f r e q u i r e d Disconnect and t e m p o r a r i l y stow SRC and camera magazine P r e p a r e f o r t r a n s f e r of documented sample SRC: a. P u l l LEC lower l i n e t o t r a n s f e r LEC hooks t o surface b. With LEC hooks i n hand, walk t o SRC on MESA c. Attach LEC lower hook t o SRC t o p - l e f t f r o n t b r a c k e t and l o c k hook d. A t t a c h upper ( r i g h t ) hook t o SRC t o p - r i g h t r e a r b r a c k e t and l o c k hook T r a n s f e r SRC: a. Extend loop end of LEC u n t i l s e c t i o n of s t r a p going t o A/S i s t a u t b. Grasp LEC t o p l i n e by loop g r i p �CDR - c. L i f t SRC from t a b l e d. Walk t o t h e f r o n t of t h e l a d d e r w i t h SRC suspended on LEC e. Walk away from l a d d e r ( i n +Z d i r e c t i o n ) w h i l e h o l d i n g LEC top s t r a p loop t o t r a n s f e r SRC t o A/S A s s i s t CDR, i f r e q u i r e d ~ e s t l c h e c kEMU Disconnect and t e m p o r a r i l y stow SRC XVII. CDR EVA TERMINATION Clean EMU by d u s t i n g w i t h hands and wiping o r k i c k i n g b o o t s a g a i n s t footpad Change SC FR t o 1 2 / s e c Ascend t o p l a t f o r m Disconnect LEC from ascent stage Receive and d i s c a r d end of LEC away from LM Hand end of LEC through h a t c h t o CDR Ingress A s s i s t CDR, i f r e q u i r e d J e t t i s o n ECS c a n i s t e r and b r a c k e t , OPS b r a c k e t s (adapt e r s ) , 3 a r m r e s t s , bag of used u r i n e bags Close h a t c h Repressurize cabin �SECTION 4.0 ALTERNATE AND CONTINGENT PLANS �4.0 ALTERNATE AND CONTINGENT PLANS 4.1 Alternate EVA (With S-band Erectable Antenna ~eployment) An alternate timeline is presented for the situation in which deployment of the S-band erectable antenna is required. Such a situation will occur if the Goldstone or Parkes (~ustralia) 210-foot antennas are not in view and the communications capability with the LM steerablel85-foot antenna combination is not sufficient to simultaneously obtain acceptable W coverage and voice-biomedical and telemetry data. Thus, due to the present uncertainty of the communications capability - possible unsatisfactory equipment performance and/or contingencies which may cause mission event times to vary so that a 210-foot antenna is not in view, the erectable antenna will be carried on the mission and a real time decision made to deploy or not deploy it, i.e., follow the alternate or the nominal timeline. With the addition of the erectable antenna deployment, the major impact to the timeline is the reduction of time available for the documented sample collection. Also, for the alternate timeline, the LMP must delay his egress to switch to the erectable antenna after the CDR has deployed it. �4.1.2 WITH DEPLOYMENT OF S-BAND ERECTABLE ANTENNA SUMMARY TIMELINE ALTERNATE LUNAR SURFACE EVA b t r r ~ v ~ corm r a rvr I I �1.50 2 a00 2r10 2.20 2.40 1.30 ...t..,..r*............... ...................................................... ................................................. z; I P ~ CSI o o c u r r r r r o s ~ u r r rc o r r c c r ~ o r LY* *.ESTPMOIO ng .OVU6MT 1 S11C *l..I C L O I I . " I .OCPLW LI'EXP. .IOIO I I I ElKlUL.IS ursrm 0 r o* . . j 1c. TO rue 0 5 Ale& o"0,r SlYPLI I c ~ ~ t c r ~ o r *lclalCVE sru L ,L". , " I . , Slit ' 11~. t o OZPLOI .KROl 01 .. 1.50 snrr ICLOSIY. .cL~." I E Y 1 ICRYIWIIO~ CYU YYPLE ."*I101 L ~ r c a c s sc r s l m ! 0C"rcl IOOLS ru .OUK.TC b c o r ~ e r SIYOLES .PAC" YYeLIs Rwros 2.00 CWIPYIII marc* U141SS Cllll I I I I I I I 7U.C PASSNC S C l S W U P . 1 C.011 *JElItSOll .SCCUIC j SCI ,IIST.RIOlO .nr.uc 0s C S. e n n s r c a o r sac I Am0 S f O l 5% LADDIm *t.Cacss I *CLOSC EYY *A%tW I CWUO. o o c v v c n l t o wrrrr c m r r c r ~ o m * m v c l V L l SIC 1 0 .CLCA# AMD SIOLL I * S T 0 1 LLSCC r l l Y Y O T O S.r.LImG *rcr*re wuprc (1YEl.S t~.hvra f::rt;it*m8&L;M~C PDros 2.10 . I I . i I sra crvenr lltCCIYt u.cul"c 8 SIW V C . jI bI ltCElVE sac 2 rJ0 2.30 2.40 �4.1.3 ALTERNATE TIMELINE LUNAR SURFACE EVA CDR HRtMIN LMP - LMP - CDR - II + %R MONITOR ACTIVITY PLAY OUT LEC MOVE TO POSITION AND RELEASE MESA 1 I I t + TV ON FOR CHECK* START SEQUENCE CAMERA (SC) + DESCEND TO FOOTPAD CHECK ASCENT PROCEDURES PLAY O ~ LEC T I TURN TV ON '(AND OFF)* CHANGE SC FR TO 24/SEC I CHANGE SC FR TO 121SEC STOW LEC T STEP TO SURFACE RESTICHECK EMU 4- + I T VISUALLY MONITOR CDR A C T I V I T Y PROVIDE CHECKLIST ASSISTANCE CHECK AND DISCUSS BALANCElSTABIL I T Y WALKING CAPABILITY *TV LEFT ON I F SATISFACTORY 1 , TELEMETRY AND CHANGE SC F I L M MAG VOICE-BIOMED CHANGE FR, TO 6/SEC 1- DATA RECEIVED A II I CDR LEC ' MISSION I APOLLO 11 I EDITION FINAL I 1 DATE 1 JUNE 27, 1 9 6 9 MISSION TIME 112+30 - 112+54 I DAY/ REV 5/19 I W6E 1 of 7 I �ALTERNATE TIMELINE CDR HRtMIN LMP T + RESTICHECK EMU I I 6 T DEPLOY HANDLE I EXTEND BAG COLLECT SAMPLE 4DETACH BAG AND LMP - REMOVE S-BAND ERECTABLE AIITEliNA FROM S/C CHECK LM-L AND EMU $TART sc t UNSTOW CSC AND - CDR II CtiECK LM AND EMU I t CHANGE CARRY ANTENNA TO DEPLOYMEiVT S I T E SC% TO B/SEC I MONITOR CDR ACTIVITY t ORIENT ANTEIIIjA REMOVE TOP CAP DISCARD HANDLE -L I I STOW SAMPLE t I TRANSFER S T I L L CAMERA TO SURFACE PROVIDE CHECKLIST ASSISTANCt EXTEND MAST AND LEGS PREPARE FOR CAMERA TRANSFER ASSIST CDR C I + REMOVE THERMAL COVER AND L I F T ANT. ONTO LEGS CHANGE SC FR TO 11SEC + REMOVE DEPLOY BAR AND R I B T I P PROTECTOR t CHECK AND REPORT LM STATUS 3- I CHAijGE SC FR TO l / S k C OPEN ANTENNA D I S H I t MONITOR CDR ACTIVITY PROVIDE CHECKLIST ASSISTANCE t CHECK TERRAIii ANij LIGHTING t REMOVE CABLE FROM MESA MONITOR CDR A C T I V I T Y I 1, MISSION AF'OLLO 11 I I EDITION FINAL I I I DATE JUNE27,1969 MISSION TIME 112+54-113+18 I DAY/ IW 5/20 I PAOE 2 of 7 �ALTERNATE TIMELINE CDR - LMP - LMP CDR - II T t T ATTACH CABLE TO ANTENNA STEP TO SURFACE REST/CHECK EMU CHANGE SC F I L M MAG. t 1 ROUGH ALIGN ANTENNA I PREPARE MESA FOR TV DEPLOYMENT I MONITOR CDR A C T I V I T Y CHECK BALANCE/STABIL I T Y I REMOVE TRIPOD -1 I CHANGE FROM WA TO L D LENS S-BAND T ~ I L U N A RSTAY TURN ~ T VON CHECK COMM, LM, AND EMU DETERMINE "GO" FOR EVA PLACE SPARE CAMERA ON L L F L O O R REORIENT SC REST/CHECK COMM AND EMU I T + REMOVE CAMERA AND PLACE ON TRIPOD + CARRY TV TO DEPLOY S I T E MISSWN 1 EDITION FINAL I I JUNE 4 + MOVE NEAR LMP REST/CHECK EMU 27, 1969 REMOVE SWC' FROM MESADEPLOY I N SUNLIGHT + P H O T L SWC I DATE ERECT SRC TABLE PLACE TV FOR SUB. EVA CHECK ASCENT PROCEDURE rC, rC, t TAKE FAST SCAN PANORAMA OR SEVERAL POINTS OF, INTEREST t PERFORM COMM CHECK I I + + MONITOR AND DESCEND TO PAD PHOTO LMP PULL TV CABLE FROM MESA t MOVE THRU HATCH CHECK INGRESS PROCEDURE MONITOR AND PHOTO EGRESS APOLLO 11 I DETERMINE WALKING C A P A B I L I T Y MISSION TIME 113+18 - 113+42 I DAY1RN 5 /20 1 1 PAGE 3 of 7 i �ALTERNATE TIMELINE LMP PLACE CAME$ ON MESA PREPARE 'MESA FOR BULK SAMPLE COLLECTION t t PREPARE ALHT AND SRC LIGHTING/VISIBILITY AND TERRAIN I N SHADOW EVALUATE AND REPORT EVA CAPABILITY AND EFFECTS ON SURFACE (TETHER CAMERA WHEN REQUIRED) REST/CHECK EMU PHOTO QUAD I t I PACK SRC EVALUATE AND REPORT LIGHTING/VISIBILITY AND TERRAIN I N SUNLIGHT REPORT STATUS AND PHOTO +Z GEAR PHOTO BULK SAMPLE AREA I t REMOVE ALSCC FROM MESA AND DEPLOY CONNECT LEC I MISSION APOLLO 11 I I CARRY ' ALSCC REPORT STATUS QUADI I V EVALUATE AND REPORT LIGHTING/VISIBILITY AND TERRAIN AT SHADOW EDGE COLLECT ROCKS AND LOOSE MATERIAL 1. I I REPORT' STATUS +Y GEAR I I EDITION FINAL I PHOTO + EVALUATE T E R R A I N / V I S I B I L . I T Y TAKE PHOTO PANORAMA TAKE CLOSE-UP PHOTOS k I DATE ( JUNE 27, 1969 M I S S I O N TIME 113+42 - 114+06 I t I t PHOTO QUAD I V DAY/ REV 5/20 + Y GEAR I t TAKE PHOTO PANORAMA /I. I PAGE 4 of 7 1 �A L T E R N A TTIMELINE E LMP - CDR - I, PHOTO QUAD I11 CARRY C A ~ E R A STO DEPLOY S I T E REPORT POSITION FROM LM CDR LMP - 2: REPORT STATUS QUAD I11 I I t t 1 REPORT STATUS -Z GEAR PHOTO -Z GEAR + I CARRY PSE TO DEPLOY S I T E I t TRANSFER CAMERA TO CDR t I REPORT STATUS DEPLOY PSE PHOTO L R ~ OPEN SEQ BAY DOOR I I AND PHOTO QUAD 11- I' T PHOTO EASEP OFFLOAD MOVE TO PSE t t REPORT STATUS AND PHOTO -Y GEAR + PHOTO PSE + MOVE BULK SRC TO STRUTS OR FOOTPAD RESTIPH'OTO LMP TAKE CLOSE-UP PHOTOS REMOVE ALSCC F I L M AND STOW I N S U I T I DEPLOY S I T E APOLLO 11 1 MOVE MESA RESTICHECK EMU MOVE TO QUAD I V . I PHOTO EASEP OFFLOAD TAKE CLOSE-UP PHOTOS I TAKE CLOSE-UP PHOTOS REMOVE PACKAGE 2 ( L R ~ ) TAKE PHOTO PANORAMA MISSION t T REMOVE PACKAGE 1 (PSE) EDITION FINAL I 1 PREPARE DS SRC AND SAMPLING EQUIPMENT L I DATE JUNE 27, 1 9 6 9 MISSION TIME 114+06 - 114+30 I DAY/R€V 5/20 I PAG€ 5 of 7 I �r ALTERNATE TIMELINE LMP &C -L TETHER SA%E LMP - II ASCEND TO PLATFORM t BAG TO LMP COLLECT CORE TUBE SAMPLE UNSTOW GNOMON SELECT DS AREA MOVE TO DS AREA PHOTO DS AREA + LI t INGRESS I CHECK LM A N D EMU REMOVE S T I L L CAMERA MAGAZINE AND CONNECT TO LEC 1 T I REORIENT CAMERA DESCRIBE AND COLLECT SAMPLES . PHOTO SAMPLES AND SAMPLE AREA ASSIST LMP I t. 4- MOVE TO MESA PLACE SAMPLES I N SRC RETRIEVE AND STOQW C MOVE TO MESA PLACE TOOLS I N ETB PACK SRC CLOSE AND SEA; SRC MOVE TO' LADDER CLEAN EMU MISSION I APOLLO 11 1 I TRANSFER BULK SAMPLE SRC AND CAMERA MAG. I- 1 EDITION FINAL - I DATE C t DISCONNECT AND STOW SRC AND CAMERA MAG. REST/CHECK EMU I LOWER LEC I I JUNE 27, 1969 ASSIST 'CDR, I F REQUIRED 1 MISSION 114+30 - 114+54 DAY! REV 5/20-21 I PAOL 6 of 7 I �LMP CDR I JETTISON EQUIPMENT CLOSE HATCH 1 '"f CABIN REPRESS �4.1.4 Detailed Procedures Refer t o t h e Nominal Lunar EVA Detailed Procedures Section 3.5, f o r t h e procedures which precede t h e S-band Erectable Antenna Deployment. LMP - CDR - S-BAND ERECTABLE ANTENNA DEPLOYMENT Transfer antenna t o deployment s i t e : . a. Walk t o antenna stowage p o s i t i o n ( ~ u a dI ) . . b . Remove thermal s h i e l d c . Remove Velcro s t r a p s and p u l l t o r e l e a s e p i n s a t base of antenna d. Grasp antenna- by deployment . "shimmy" b a r and folded l i f t handle ' e . P u l l antenna o u t and down by l i f t handle t o c l e a r LM s t r u c ture f . Hold antenna by deployment b a r and deploy f o l d e d l i f t handle by p u l l i n g handle o u t of stowage d e t e n t and down t o ' l o c k e d position g. Rotate antenna t o h o r i z o n t a l p o s i t i o n and c a r r y t h e antenna t o t h e deployment s i t e by t h e . shimmy b a r (NOTE: The s i t e t o be used should provide a c l e a r view of Earth and b e approximately 20 f e e t from t h e MESA). h. Place - t h e antenna down with t h e bottom antenna handle r e s t i n g . . on t h e s u r f a c e and t h e orientat i o n arrow on top cap pointing , t o Earth. , When CDR moves i n t o SC f i e l d of view, change SC frame r a t e t o 6/sec �CDR - Remove t o p cap: a. b. c. Release each of t h e t h r e e l e g clamps by r o t a t i n g them out and down Depress t h e t h r e e l e g t i p s and push them r a d i a l l y outward t o f r e e t h e antenna t o p cap Discard metal t o p cap and foam piece i n a r e a away from t h e LM Raise antenna mast : While holding t h e antenna vert i c a l , grasp antenna horn t o p p l a t e and r a i s e t h e first s e c t i o n of t h e antenna feed support. (insure t h e f i r s t s e c t i o n only i s deploying by applying a 2-finger pressure on o u t e r mast section. The outer s e c t i o n has orange stripes. ) Do not touch h e l i x eleCAUTION: ----ment when extending feed assembly .b. Check f i r s t s e c t i o n f u l l y deployed and locked i n detent c. Extend t h e second antenna feed s u p p o r t , s e c t i o n i n t h e same manner a s t h e f i r s t . Check t h e second s e c t i o n f u l l y extended and locked i n detent. a. Deploy t r i p o d : a. b. Extend antenna l e g s by placing 2 f i n g e r s about t h e l e g s e c t i o n and applying f o r c e against loops on e i t h e r s i d e of l e g . Continue t o extend each l e g s e c t i o n t o t h e proper' l e n g t h , i .e., t h e proper p a i n t r i n g and lock with clamps. Check adequacy of each l e g lock Check antenna point toward e a r t h by arrow on r i b programmer IMP - �IMP - CDR - Move around t o t h e r i g h t i n t o t h e antenna l i f t i n g position by t h e shimmy bar P u l l each of t h r e e Velcro l e g retension s t r a p s and l e t the l e g s f a l l outward t o a horizontal position on t h e surface Remove thermal covering from antenna and discard away from LM L i f t t h e antenna from t h e surface using both hands on t h e shi,pmy bar u n t i l t h e antenna i s high enough t o permit t h e crewmember t o . g r a s p the lift handle While holding t h e antenna a l o f t with one hand, grasp l i f t handle with other hand L i f t t h e antenna t o t h e high detent position Check each l e g locked securely i n detent by holding the antenna a l o f t with one hand,and pushing outboard on the l e g s individually Set antenna on surface Release p u l l pin fastener a t base of shimmy bar. P u l l deployment bar down and away from antenna Discard bar i n t h e area away from the Firmly implant each l e g i n t o surface ' Open antenna r e f l e c t o r : a, b. c. d. e. Remove r i b t i p protector and allow it t o s l i d e down antenna l e g t o surface Uncoil antenna r e f l e c t o r r e l e a s e cable from around antenna. Hold cable t a u t and i n s t r a i g h t l i n e t o plunger Remove release t r i g g e r guard pin and discard i n area away from IM Graps an antenna l e g with f r e e hand and position s e l f a t arms length from l e g With head down, squeeze release t r i g g e r t o deploy antenna dish. �CDR - IMF - Attach antenna cable: Walk t o f r o n t of MESA, a d j u s t MESA i f necessary P u l l Velcro s t r a p s t o f r e e l e f t s i d e of thermal blanket Unfold lef't s i d e of blanket t o permit easy access t o cable Release antenna cable connector by p u l l i n g Velcro t a b and snap f r e e Grasp cable connector and pass t h e connector under t h e MESA support s t r a p With cable connector i n hand, walk t o t h e lef't of t h e antenna Walk p a s t t h e antenna and deploy t h e cable completely ( u n t i l black and white s t r i p e d section visible ) Walk t o antenna ,Connect antenna cable by mating t h e two connector p a r t s t u r n i n g t h e outer p a r t clockwise a s viewed from cable end Change SC FR t o l / s e c - Rough a l i g n antenna: a. b. c. d. e. Move around antenna l e g t o rough antenna alignment p o s i t i o n Unstow alignment crank by pushing down and away on crank handle Uncoil crank cable by passing crank wound and behind t h e ant enna base Rough a l i g n antenna i n p i t c h (CCW r o t a t i o n of t h e handle p i t c h e s t h e antenna down) Rough align'antenna i n azimuth. Pull antenna crank out from housing then r o t a t e handcrank t o change antenna azimuth Change SC f i l m magazine when necessary �Fine a l i g n antenna: a. b. c . Press each l e g i n t o surface Check antenna alignment by s i g h t i n g along antenna mast and using o p t i c a l alignment s i g h t Fine a l i g n antenna, a s required, by using remote c o n t r o l crankhandle "in" f o r p i t c h and "out" f o r azimuth Rest-check communications and EMU systems. Take one photo of antenna Switch t o e r e c t a b l e antennaS-band s e l e c t o r t o "Lunar stay" (FM, Mode 10) Perform communications check. Check s i g n a l s t r e n g t h indication > 1.0. Verify voice and telemetry with MSFN. Check LM and EMU systems. Determine "GO" f o r EVA Refer t o t h e Nominal EVA procedures, Section 3 . 5 , f o r t h e LMP I n i t i a l EVA procedures. �4.2 Contingent EVA 1 - Minimum Time, One Man 4.2.1 Description and Rationale For various reasons, on the first lunar landing mission only a very limited time may be available to accomplish the,EVA.* For such a situation the choice of objectives are, first, those with the highest priority and, secondly, those which can be accomplished in a Short period of time and do not require the accomplishment of a previous task. The timeline presented here, referred to as the Contingent EVA 1 or Minimum-Time, One-Man EVA, is to optimize the accomplishment of the choice of objectives by providing the maximum data return for the minimum amount of time expended. ( ~ M n A timeline of approximately 49 minutes). There are several other considerations which enter into the selection of the tasks and the procedural detail of the activities for a minimum time EVA. As this will be an unplanned or contingent EVA, it is desirable to have the procedures and sequence of events closely related to the nominal. Either crewman should be equally capable of conducting the desired tasks and contributing to the data returned. And in general, to achieve the maximum diversified data collection, the crewman on the surface will not go into the procedural detail, particularly with verbal descriptions, as he is expected to in the nominal timeline. In this contingent EVA, for the environmental familiarization, the crewman will spend only enough time to assure himself that he can safely proceed with the EVA. After the contingency sample collection he will continue to become more adapted to the new environment as he conducts a limited EVA evaluation. PrimariLy, this EVA evaluation will involve a brief investigation to determine an astronaut's general capabilities or limitations for conducting EVA tasks within the lunar environment. Photographs taken during this evaluation will be a postflight aid to the crewman's recall and the documentation of this activity. A limited LM inspection, with very brief comments and several documentary photographs, can be conducted for the forward half of the spacecraft within a few minutes. To conclude the surface activity the crewman will take a photographic panorama and possibly a few additional photographs of documentary value. In conclusion it should be mentioned that the crewman's surface activity will be confined to an area where he can be constantly monitored by and in communications with the crewman inside the LM. Practically all of the activity can be documented with the sequence camera, and, if the communications capability exists, with the TV. Also, there should be sufficient time and activity for a thorough PLSS analysis. The final Flight Mission Rules for Apollo 11 wil1,govern the selection of the crewman to egress and the EVA he will accomplish. . . ' 86 �4.2.2 T I M E SCALE q C O W N011nr D HODUU ( . .-. E H I LllL SUMMARY TIMELINE CONTINGENT EVA I I0 . ACTIVITY C S M l l M COMM I MCC-H ACTIVlTV I P A R A T C S YUOM UOCKS W S T N l T V t CWRDIMTED TASKS I I. F I ~ LVRE-LVA OI(MTIDUS #DEPRESS FROM 3.) PSI b SEQlENX CALTRA C M R A Q ~ C W E M A C E b FRAME W ~ c w r n ~ c r C . INITIAL N A tcouu T V COVERAGE 1FRAYVYC I1 MINIMUM TIME, ONE MAN COMMANDER ACllVlTY cnrcr ORELEASE Y Y I 0.LRFORU C l U L SYSlLYS CHECKS I 12 F R A U E ~ C . ~DETERUIML GO FOI EVA 24 F R A Y E V I f C 0 1CcoveACE BXgl Y U I C M ~ E OfCTIVATE SEQUENCE CAULMA LM PILOT ACTIVITY IDEPLOV LEE AS SAFETY UOUITOR I l M E SCALE OASCEND LADDER OCOLLECT SAMPLE ODETACH B I C L GISCUD MMDLE OIYCRESS U B I N .+z ORESIXMECI: EMU . OP(IWIDE CHECKLIST ASSISTA*CE I I OP((OT0CRAPWI DA , @ . I +.Y CLU OJETTISOM EPUINENT .SECURE MTCH 1" OREPRESSURIZE CABIN 1-1 GEAR f REV. YLRCH I ITRAMSFER STILL CAYERA 1 0 SURFACE 4.2.2 OR: HENORICKS CH SUMMARY 1IMELINE c o m r l m c r n EVA I (US% Y M . 1969 � 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_000072 Title A name given to the resource Final Apollo 11 Lunar Surface Operations Plan. Description An account of the resource Prepared by the Lunar Surface Operations Office, Mission Operations Branch, Flight Crew Support Division. Creator An entity primarily responsible for making the resource Wood, William H., Jr. Manned Spacecraft Center (U.S.) Date A point or period of time associated with an event in the lifecycle of the resource 1969-06-27 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Apollo 11 (Spacecraft) Lunar surface vehicles Project Apollo (U.S.) Saturn Project (U.S.) Saturn launch vehicles Space flight to the moon Space vehicles--Moon--Landing Type The nature or genre of the resource Reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 32, Folder 10 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/211/14910/lincoln.mill.store.03162025.jpg 62ef2ee17a5a77c91256bf2d98899543 Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. 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 Lincoln Mill company store, 03/16/2025 Creator An entity primarily responsible for making the resource Woodward, Aimee F. Identifier An unambiguous reference to the resource within a given context linoln.mill.store.03162025 Description An account of the resource Personal photograph of Aimee Woodward. The Lincoln Mill company store building is currently used as a commercial space. Date A point or period of time associated with an event in the lifecycle of the resource 2025-03-16 Format The file format, physical medium, or dimensions of the resource Photo, Print, Drawing Source A related resource from which the described resource is derived 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. https://digitalprojects.uah.edu/files/original/211/14877/lincoln.mill.villagehousing.presentday.jpg 361f8660f3a9baa237724baecaaf3c96 Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. 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/. Creator An entity primarily responsible for making the resource Woodward, Aimee F. Identifier An unambiguous reference to the resource within a given context lincoln.mill.villagehousing.presentday Description An account of the resource These homes in Lincoln Mill Village are located behind Lincoln School. The houses were built to provide accommodation for mill workers. The photograph was taken in March 2025. Date A point or period of time associated with an event in the lifecycle of the resource 2025-03-16 Source A related resource from which the described resource is derived 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. Title A name given to the resource Lincoln Mill village housing, March 2025. https://digitalprojects.uah.edu/files/original/211/14909/lincoln.mill.school.presentday.jpg 4727122141a034f3c90e8a5046c7da2c Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. 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 Lincoln Academy, formerly known as Lincoln School. Creator An entity primarily responsible for making the resource Woodward, Aimee F. Identifier An unambiguous reference to the resource within a given context lincoln.mill.school.presentday Description An account of the resource Lincoln Academy now occupies the building known to locals as the Lincoln School. The school, as it stands, was constructed in 1929. Date A point or period of time associated with an event in the lifecycle of the resource 2025-03-16 Source A related resource from which the described resource is derived 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. https://digitalprojects.uah.edu/files/original/211/14984/lincoln.mill.03162025.jpg 501012eee0a4873d95f6b57ced302568 Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. 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 Lincoln Mill, 2025-03-16 Creator An entity primarily responsible for making the resource Woodward, Aimee F. Identifier An unambiguous reference to the resource within a given context lincoln.mill.03162025 Description An account of the resource Lincoln Mill has transitioned from a textile mill to a military complex and now serves as a vibrant cultural and commercial space. Date A point or period of time associated with an event in the lifecycle of the resource 2025-03-16 Format The file format, physical medium, or dimensions of the resource Photo, Print, Drawing Source A related resource from which the described resource is derived 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. https://digitalprojects.uah.edu/files/original/4/4184/spc_nick_000291_000291.pdf 504a29aa11a73961edd4f7ce93acf732 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 Col. John C. Nickerson, Jr. Papers 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_nick_000291_000291 Title A name given to the resource Letter to Colonel John C. Nickerson, Jr. from Colonel Robert C. Works. Description An account of the resource Works expresses sympathy toward Nickerson and the situation he is in asking, "�what's happening to the Army?" Works offers a character witness or any deposition or testimony that would help his case. Creator An entity primarily responsible for making the resource Works, Robert C. Date A point or period of time associated with an event in the lifecycle of the resource 1957-02-08 Temporal Coverage Temporal characteristics of the resource. 1950-1959 Subject The topic of the resource Courts-martial and courts of inquiry--United States Defense information, Classified Intermediate-range ballistic missiles Jupiter missile Leaks (Disclosure of information) Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Correspondence Text Source A related resource from which the described resource is derived Col. John C. Nickerson, Jr. Papers Box 1, Series 1, Folder 4 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_nick_2021_03 https://digitalprojects.uah.edu/files/original/207/14744/The_Selma_Times_Journal_1995_11_20_1_sharedrights.jpg ebfaadbc3df54da2b16c63ff8f3e83dd 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 RCEU Faith Based AIDS Responses in 1980s and 1990s Alabama Creator An entity primarily responsible for making the resource Morgon Newquist 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 The_Selma_Times_Journal_1995_11_20_1_sharedrights Title A name given to the resource Shared Rights, Shared Responsibilities World AIDS Day in the Selma Times Journal Source A related resource from which the described resource is derived The Selma Times Journal, Newspapers.com, Ancestry.com (LLC) 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 A graphic design image for World AIDS Day in 1995 with the slogan "Shared Rights, Shared Responsibilities." that appeared in an issue of the Selma Times Journal. This is from a digitization of the newspaper. The image is from a national campaign and appeared in the Selma Times Journal. Creator An entity primarily responsible for making the resource World Health Organization Publisher An entity responsible for making the resource available Selma times journal Date A point or period of time associated with an event in the lifecycle of the resource 1995-11-20 Temporal Coverage Temporal characteristics of the resource. 1990-1999 Subject The topic of the resource AIDS (Disease) HIV (Viruses) AIDS (Disease) in mass media AIDS (Disease)--History World AIDS day Type The nature or genre of the resource Newspapers Clippings https://digitalprojects.uah.edu/files/original/128/8744/r06_01-03.pdf e52891ea184b3ba787f7d17e22a5be7d 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 Series 06: Pettus Family Title A name given to the resource Series 06: Pettus Family Still Image A static visual representation. Examples include paintings, drawings, graphic designs, plans and maps. Recommended best practice is to assign the type Text to images of textual materials. 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 r06_01-03 Source A related resource from which the described resource is derived Series 6, Box 1, Folder 3 Title A name given to the resource Wright, Hannah McCool [letter] to Alice Pettus, 1931 Relation A related resource r06-211007 Description An account of the resource A single letter of correspondence from Hannah McCord Wright Creator An entity primarily responsible for making the resource Wright, Hannah McCord Date A point or period of time associated with an event in the lifecycle of the resource 1931-01 Temporal Coverage Temporal characteristics of the resource. 1930-1939 Subject The topic of the resource Letters Type The nature or genre of the resource Correspondence Is Part Of A related resource in which the described resource is physically or logically included. Frances Cabaniss Roberts Collection 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. https://digitalprojects.uah.edu/files/original/213/15031/wsig-history-month.pdf 7a06cb0561d7b8e39ccf9b4796ead713 PDF Text Text � 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 RCEU Documenting the History of UAH’s Women’s, Gender, and Sexuality Studies Program Title A name given to the resource RCEU Documenting the History of UAH’s Women’s, Gender, and Sexuality Studies Program Description An account of the resource Documenting the history and evolution of UAH's Women's, Gender, and Sexuality Studies program. Covers the conception of the program in 1995 and how the program evolved throughout its current iteration. 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 "WSIG kicks off National Women's History month activities" Creator An entity primarily responsible for making the resource WSIG Subject The topic of the resource Women's studies Identifier An unambiguous reference to the resource within a given context "WSIG kicks off National Women's History month activities" Description An account of the resource Newsletter describing WSIG activities for women's history month 1997. Date A point or period of time associated with an event in the lifecycle of the resource Unknown Source A related resource from which the described resource is derived Women's Studies 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. Format The file format, physical medium, or dimensions of the resource newsletter https://digitalprojects.uah.edu/files/original/20/10629/rolenasamsfcmanufeng_071207105624.pdf 0b8e436a6f952b827a1ae22b83379bf2 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 rolenasamsfcmanufeng_071207105624.pdf spc_stnv_000669 Title A name given to the resource "The role of the NASA-MSFC Manufacturing Engineering Laboratory in the development of space projects." Description An account of the resource For presentation at the Aerospace Industries Association of America (AIA) Manufacturing Engineering Committee Meeting. Discusses the role the NASA Engineering Laboratory has had on NASA projects in the form of vehicles and smaller projects. Creator An entity primarily responsible for making the resource Wuenscher, Hans F. Date A point or period of time associated with an event in the lifecycle of the resource 1964-11-12 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project George C. Marshall Space Flight Center. Manufacturing Engineering Laboratory Space vehicles--Design and construction Space sciences Aerospace industries--United States Type The nature or genre of the resource Text Presentations Source A related resource from which the described resource is derived Saturn V Collection Box 12, Folder 39 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_000650_000674 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/17056 https://digitalprojects.uah.edu/files/original/36/4541/loc_hutc_000167_000175.pdf 60c151fefb4bf3ff270344d1d50c4190 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 Eleanor Hutchens Collection Identifier An unambiguous reference to the resource within a given context Eleanor Hutchens Collection Description An account of the resource Eleanor Newman Hutchens (October 9, 1919 to November 9, 2016) attended Agnes Scott College in Decatur, Georgia, majoring in English and Greek. After receiving her B.A. in 1940, she attended the University of Pennsylvania, acquiring an M.A. and Ph.D. in English literature (“Eleanor Hutchens - Obituary”). Hutchens first held a part-time teaching position at the University of Alabama in Huntsville in 1955, then joined the faculty with a full-time position in 1957. She taught English, her specialties the English novel, literary criticism, and 18th century literature. Hutchens also chaired the steering committee “for its initial accreditation and the first committee for the selection of majors,” and served as the first elected president of the Faculty Senate. She moved to Agnes Scott College in 1961, remaining there until 1966. She eventually returned to UAH and remained a member of its English department until her retirement in 1979 (“Eleanor Hutchens - Obituary”). Hutchens wrote prolifically over and after her career, publishing Irony in Tom Jones, Writing to Be Read, and “numerous articles in national and international journals” (“Eleanor Hutchens - Obituary”). Hutchens was very active even outside of her academic career, serving as "president of the Huntsville Hotel Company, owner of the Russell [sic] Erskine Hotel, and as a director of the Huntsville Land Company, the West Huntsville Land Company, and the Mountain Heights Development Company.” She was "a founder and charter member of the board of Randolph School," a board member of the Huntsville Public Library and the Huntsville Symphony, and "an active member of the [Episcopalian] Church of Nativity.” Hutchens was also a member of "the Historic Huntsville Foundation, the Huntsville Historical Society, the Botanical Garden, the Burritt Museum of Art, the Huntsville Museum of Art, and the Friends of the Huntsville Public Library” (“Eleanor Hutchens - Obituary”). Sources “Eleanor Hutchens - Obituary.” Legacy.com, 3 Jan. 2019, www.legacy.com/obituaries/name/eleanor-hutchens-obituary?pid=182447617. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/156">View the Eleanor Hutchens Collection finding aid in 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 loc_hutc_000167_000175 Title A name given to the resource Correspondence including Dr. John A. Wyeth. Description An account of the resource Dr. Wyeth writes to a "friend" about working, asks about Sam Russell and requests that the enclosed letter is given to him. He also asks for any information about Meck Robinson. The recipient, possibly W. P. Newman, responds that he gave the letter to Russell. He discusses their friendship and thanks Wyeth for the "Expressions of friendly, sweet, and tender miracles" for his family. He also discusses working and life struggles, calling the world "cold." The author shares various verses and personal information through his lengthy letter. The seventh and final page is missing the bottom part. The back of the final page includes a drawing, presumably by a child, and a handwritten note. Creator An entity primarily responsible for making the resource Wyeth, John A. Date A point or period of time associated with an event in the lifecycle of the resource 12/27/1907 2/19/1908 Temporal Coverage Temporal characteristics of the resource. 1900-1909 Subject The topic of the resource Friendship Letter writing Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Correspondence Text Source A related resource from which the described resource is derived Eleanor Hutchens Collection Box 3, Folder Old Family Papers 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 loc_hutc_2021_04 https://digitalprojects.uah.edu/files/original/20/1277/spc_stnv_000134.pdf 9bf6179d2378e83535ed213299be89e4 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_000134 Title A name given to the resource "Automatic Saturn V Page Test System." Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. IBM No: 65-825-1430 Description An account of the resource The abstract notes, "This paper describes the Automatic Saturn V Page Test System. The system is used to evaluate microminiature Unit Logic Device (ULD) circuits. A page is an assembly consisting of a magnesium- lithium frame, an input-output connector, test points, and multilateral printed circuit boards that interconnect the IUDs into logic circuits. The test system automatically performs tests for shorted voltages and shorted diodes, static logic function, and pulse function." Creator An entity primarily responsible for making the resource Wylie, W. D. International Business Machines Corporation. Federal Systems Division Date A point or period of time associated with an event in the lifecycle of the resource 1965-05-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Automatic test equipment Computer arithmetic and logic units Logic circuits Saturn launch vehicles Saturn Project (U.S.) Type The nature or genre of the resource Technical reports Text Source A related resource from which the described resource is derived Saturn V Collection Box 13, Folder 33 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/17125 https://digitalprojects.uah.edu/files/original/20/10379/Spaceandtheworkingwoman_061908150158.pdf 635fb5666e525168cb7f0b4c2a6281ec 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 Spaceandtheworkingwoman_061908150158.pdf spc_stnv_000834 Title A name given to the resource "Space and the working woman." Description An account of the resource Memorandum prepared for the honoring Amelia Earhart by the Zonta Club, Birmingham, Alabama. Creator An entity primarily responsible for making the resource Wyss, G. L. United States. National Aeronautics and Space Administration Date A point or period of time associated with an event in the lifecycle of the resource 1969-01-18 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Women scientists Employment Discrimination Space race Type The nature or genre of the resource Text Memorandums Source A related resource from which the described resource is derived Saturn V Collection Box 25, Folder 18 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_000825_000849 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/17826 https://digitalprojects.uah.edu/files/original/73/1502/spc_youn_000001_01.mp3 beb55637fcef61c35c485d15d09b0c08 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 0:38:33 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_youn_000001_01 spc_youn_000001_02 MC_8_001 Title A name given to the resource Don Brevik- Rocketdyne engineer. Creator An entity primarily responsible for making the resource Young, Anthony Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/73/1503/spc_youn_000002_01.mp3 a2044f5153b62a8bd3e48f9f9381a6bd https://digitalprojects.uah.edu/files/original/73/1503/spc_youn_000002_02.mp3 7f463748ce69de4ad806d1ece576096f 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 1:01:48 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_youn_000002_01 spc_youn_000002_02 MC_8_002 Title A name given to the resource Richard Brown- MSFC. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2007-04-12 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/73/1504/spc_youn_000003_01.mp3 5480eefd72050d943f65bcfd5202d64a https://digitalprojects.uah.edu/files/original/73/1504/spc_youn_000003_02.mp3 f74137948eec6c7e0c578c80542aaf33 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 0:43:57 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_youn_000003_01 spc_youn_000003_02 MC_8_003 Title A name given to the resource Richard Brown- MSFC. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2007-04-12 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/73/1505/spc_youn_000004_01.mp3 e94dee0df47353267f5243bdc2726602 https://digitalprojects.uah.edu/files/original/73/1505/spc_youn_000004_02.mp3 5fdc4178e32341bcbb9b1a36ca5f2ddc 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 0:50:27 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_youn_000004_01 spc_youn_000004_02 MC_8_004 Title A name given to the resource Frank Steward- MSFC. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2007-04-11 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/73/1506/spc_youn_000005_01.mp3 154deb596c8befcca8d14da7a02b47e4 https://digitalprojects.uah.edu/files/original/73/1506/spc_youn_000005_02.mp3 d37bc89264e356102c7d206b02a5e61b 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 1:01:41 OHMS Object This field contains the OHMS Hyperlink (link to the XML file within the OHMS Viewer) http://libarchstor2.uah.edu/ohms-viewer/render.php?cachefile=spc_youn_000005_01.xml 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_youn_000005_01 spc_youn_000005_02 MC_8_005 Title A name given to the resource Konrad Dannenberg- MSFC. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2006-06-23 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History https://digitalprojects.uah.edu/files/original/73/1507/spc_youn_000006_01.mp3 06b69c576754f564dff76f531bd1c55b 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 Anthony Young Collection Title A name given to the resource Anthony Young Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/1" target="_blank" rel="noreferrer noopener">View the Anthony Young Collection finding aid in ArchivesSpace</a> Description An account of the resource Anthony Young was born in 1950. He graduated from Pratt Institute with a B.A. degree in Industrial Design. Mr. Young has worked for over twenty years in the aerospace industries. He is an author, a scientist, and aerospace historian. Oral History A resource containing historical information obtained in interviews with persons having firsthand knowledge. Duration Length of time involved (seconds, minutes, hours, days, class periods, etc.) 0:16:19 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_youn_000006_01 spc_youn_000006_02 MC_8_006 Title A name given to the resource Harold C. Hall- MSFC. Creator An entity primarily responsible for making the resource Young, Anthony Date A point or period of time associated with an event in the lifecycle of the resource 2007-04-12 Temporal Coverage Temporal characteristics of the resource. 2000-2009 Format The file format, physical medium, or dimensions of the resource Audiocassettes Type The nature or genre of the resource Interviews Audio Source A related resource from which the described resource is derived Young 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 clir_grant_audio_metadata Oral History