192 20 8242 https://digitalprojects.uah.edu/files/original/20/1139/spc_stnv_000055.pdf a3ffc30c2c9f010d1c077286206b49e3 PDF Text Text A Hybrid Simulation for Dynamic Verif icatio of Saturn Guidance and Control Subsystem: �IBM NO. 68-U6O-0013 A HYBRID SIMULATION FOR DYNAMIC VERIFICATION O F SATURN GUIDANCE AND CONTROL SUBSYSTEMS . Ronald T Patray May 15, 1968 International Business Machines Corporation Federal Systems Division Space Systems Center Huntsville, Alabama �A HYBRID SIMULATION FOR DYNAMIC VERIFICATION O F SATURN GUIDANCE AND CONTROL SUBSYSTEMS Ronald T. Patray International Business Machines Corporation Federal Systems Division Space Systems Center Huntsville , Alabama I. INTRODUCTION This paper presents a discussion of a hybrid simulation used to dynamically verify the Saturn Guidance and Control subsystems. First, the Saturn vehicle is briefly described to provide background information. The Instrument Unit (IU) is considered in more detail to give a proper setting f o r the Guidance and Flight Control (G and FC) discussion that follows. After a brief description of the actual G and FC System operation, simulation models of the G and FC components a r e considered in detail. This is followed by a discussion of the model assignment to a particular computer (digital o r analog) and justification f o r making that assignment. Finally, results of the A S - 2 0 4 / ~ ~ 1 hybrid simulation studies a r e briefly considered with mention of the actual flight data. 1 11. SATURN VEHICLE DESCRIPTION The Saturn IB, which has two propulsive stages (Slide I ) , is serving as a launch vehicle f o r the Apollo spacecraft earth orbital flight tests. These flights simulate certain studies of the lunar landing mission and provide flight 1 Some of the material in this paper is based on notes f r o m an IBM conference presentation entitled, "Digital Computer Program for Support of Hybrid Computer Simulation of Saturn Launch Vehicle, " by E. W. Snyder. �t e s t s for the spacecraft and the S-IVB/IU Stage. Each Saturn IB has a payload consisting of some combination of a Lunar Module (LM), Service Module (SM), Command Module (CM), and Launch Escape System (LES). The Saturn V, which has three stages (Slide I ) , is the launch vehicle f o r the actual lunar landing missions. For these missions the Saturn V will c a r r y a payload consisting of an LM, SM, CM, and LES. 111. INSTRUMENT UNIT The major purpose of the Instrument Unit (IU) shown in Slide 2 is to provide the Saturn vehicle with a centralized astrionics package for guidance, control, sequencing, and telemetry during boost and earth orbit, and through lunar trajectory insertion. The IU subsystems (Slide 3 ) include the Structural Portion, Guidance, Flight Control, Environmental, Instrumentation, and Electrical. A. Guidance and Flight Control Subsvstems Slide 4 lists the major components of the Guidance and Flight Control Subsystems. Included a r e the Launch Vehicle Digital Computer (LVDC), the Flight Control Computer (FCC), the ST-124 Inertial Platform, and the control accelerometer and rate gyro /control signal processor. Slide 5 shows a rough sketch depicting the closed loop operation of the Guidance and Flight Control Subsystems. Sensors on the inertial platform meas u r e the angles ( 8 ) between the inertial and body reference f r a m e s and changes in velocity along each inertial axis. These signals a r e transmitted to the LVDC-LVDA where the velocities a r e used in navigation and in computing the commanded gimbal angles (x). The actual platform gimbal angles ( 8 ) a r e differenced with the x's to give attitude e r r o r signals ($1 in the inertial platform frame. These $ 's a r e transformed to result in attitude e r r o r signals ( A qb ) in the body frame, which a r e fed to the FCC where they a r e filtered and summed with the filtered rate gyro signals to give engine actuator commands (4).The ,f3 signals drive the actuators and thus change the thrust vector orientation which in turn changes the vehicle attitude. (6) IV. DYNAMIC VERIFICATION OF THE GUIDANCE AND CONTROL SYSTEM Filters in the FCC and parameters in the LVDC flight program a r e designed to give satisfactory stability margins while maintaining good vehicle �response to guidance commands. These designs a r e determined by using linearized models and linear stability analysis techniques at a few frozen points in time. While this method of design has proved, thus f a r , to be reliable, it does not consider the effects of nonlinearities in the guidance system, nor does it consider vehicle dynamics continuously throughout boost flight. Thus, a means of dynamically checking the FCC filter design and LVDC flight program in a total system configuration under flight conditions, over all times of vehicle boost flight, was needed to ensure the nonexistence of adverse dynamic effects on the vehicle, the astronauts, and the guidance accuracy. It was decided that a system would be devised in which, except for the LVDC flight program, all components significantly affecting the vehicle dynamics would be simulated. For this task, a six degree-of -f reedom real time hybrid simulation with LVDC/LVDA flight hardware in the loop was chosen that would fully exercise the flight program and check its dynamic effects on the vehicle throughout simulated boost flight, and at the same time check the FCC filter design for vehicle stability and response. V. HYBRID SIMULATION Slide 6 shows a simplified G & FC loop for pitch and yaw. The LVDC and LVDA a r e flight-type hardware, while the Flight Control Computer, Engine Actuator, Vehicle Dynamics, Rate Gyro, Inertial Platform Assembly, and Propellant Utilization System (PU) a r e simulated on the hybrid system. Each component that significantly contributes to vehicle dynamics is described below, followed by a description of the simulation model of each component. A. Launch Vehicle Digital Computer (LVDC) 1. Actual LVDC Slide 7 depicts the Saturn V flight computer (LVDC) tasks by phase: Phase I includes the time of f i r s t stage boost. During this phase the vehicle is moving through the dense portion of the atmosphere where high aerodynamic pressure occurs. To avoid excessive structural loads caused by guidance maneuvers, no guidance constraints a r e applied. An open loop guidance scheme in the form of a time tilt program is used. Phase I1 includes the second stage boost time. The flight program during this phase uses a path adaptive guidance scheme called Iterative �Guidance Mode (IGM) in which guidance is a function of space-fixed position (F ) and velocity (G ) , ~ / m and time. This adaptive guidance scheme seeks to attain predetermined space -fixed position and velocity vectors with the consumption of a minimum amount of propellant. Phase I11 includes the f i r s t burn time of third stage boost and orbital time. IGM guidance is used during the boost portion of this phase. Phase IV includes the second burn time of third stage boost. IGM guidance is also used during this phase. Phase V includes all mission time after $-NB/IU Apollo Spacecraft separation. The LVDC/LVDA has a s inputs inertial platform gimbal angles, measured changes in velocity along each platform axis, and flight sequencing discretes. The LVDC/LVDA outputs a r e attitude-error steering commands and flight sequencing discretes. Since an actual flight type LVDC/LVDA is used in the simulation, no LVDC/LVDA model was devised. B. ST- 124 Inertial Platform Assemblv 1. Actual Platform The Inertial Platform Assembly (Slide 6) is the main sensor for guidance. At guidance reference release, which occurs a few seconds before liftoff, the platform becomes inertial (space-fixed). A resolver attached to each platform surface measures the gimbal angle ( 8 ) between the surface and vehicle axis. These resolver outputs a r e read by the LVDC flight program every 40 milliseconds. Integrating accelerometers, mounted along each axis of the platform, sense changes in measured velocities (AX,, A * ~ , A 2,) in increments of .05 m/sec. Signals representing these velocity changes automatically increment o r decrement velocity counters in the LVDA. These counters a r e read periodically by the LVDC flight program. �2. Platform Simulation Model Platform gimbal angles ( 0 ) a r e simulated by first transforming the simulated body r a t e s (Slide 6) into the inertial coordinate frame, and then integrating the resulting gimbal angle r a t e s (8). Gimbal angles a r e computed and transmitted to the LVDA at a 40-millisecond rate. (4) The platform integrating accelerometers a r e simulated in two ways: During f i r s t stage simulation, vehicle thrust is obtained through a table lookup scheme of thrust versus vehicle altitude. Thrust is then used with remaining vehicle m a s s (m,), which is computed, to obtain total vehicle acceleration . engine angles (F/mV). This acceleration is resolved through the simulated ( P ) to result in body acceleration components gB,yB, ZB). which in turn a r e transformed via the platform gimbal angles (0) into inertial platform acceleration components Wm, Y,, z,). These accelerations a r e then used to compute changes in measured platform velocity components (AX,, A A i m ) which would normally be sensed by the platform integrating accelerometers. The measured velocity changes a r e computed and transmitted through special interface equipment to the LVDA every 40 milliseconds. During the second and third stage simulation, vehicle thrust is obtained through a table lookup scheme of thrust versus Propellant Utilization System (PU) valve position, which is the output of the PU System simulation model. After vehicle thrust has been obtained, changes in the platformmeasured velocities (AX,, A , A z,) a r e derived in the same manner as in the f i r s t stage simulation. . C. Flight Control Computer (FCC) 1. Actual FCC The primary functions of the FCC a r e to provide command signals (PC) to the engine actuators and to ensure adequate vehicle stability by compensating the guidance and control loop with proper attitude e r r o r and r a t e filters. These f i l t e r s a r e implemented with passive elements. The FCC shown in Slide 6 has as inputs attitude-error steering commands ( A4's) from the LVDA and body r a t e s (4's) f r o m the body rate gyros. These inputs, when filtered in the FCC and summed, result in actuator commands (PC's)which move the engine actuator, and thus the thrust vector, to cause changes in vehicle dynamics. �2. FCC Simulation Model Slide 8 shows a simplified block diagram of the pitch control loop, including sloshing and bending models for a single engine stage. The simulated attitude and attitude rate filters a r e implemented with passive elements a s in the actual FCC. The control gains a. and a 1 a r e changed during actual and simulated flight in discrete steps to offset changes in the control moment of inertia. D. Engine Actuators 1. Actual Actuators The Saturn engine actuators, while differing in type from stage-to-stage, a r e all highly nonlinear with rate and position limits. 2 . Actuator Simulation Models Linear approximations of the engine actuators a r e used in the hybrid simulation. The transfer functions for these actuator models a r e of order three o r four, depending on the boost stage. In using these linear approximations, small engine angles (0 to 1 3 degrees) a r e assumed. Simplified nonlinear actuator models a r e presently being developed to handle more severe cases of engine movement. E. Bodv Bending Model The effects of one mode of body bending, caused by forces due to engine position ( p ) and acceleration a r e simulated in the pitch plane (Slide 8) by a second order linear model. The effects of bending (dB and A O B ) a r e sensed by the rate gyros and platform gimbals and therefore affect the guidance and control loop. (B), F. Moment Equation Model Motion of the rigid body is described by simple rotational mechanics: is equal to a moment coefficient C2 times Sin P , The attitude acceleration (4) where C2 is total thrust times the moment a r m (distance from engine gimbal to center of gravity) divided by the moment of inertia. The Hybrid Simulation �computes C2 on line from its component parts. The small angle approximation Sin P = P (radians) is used. G. Propellant Slosh Model Propellant Sloshing (LOX and LH2) effects on the vehicle attitude acceleration in the pitch plane and the Propellant Utilization System Valve Control a r e included in the simulation of the second and third stages. The inputs that cause major sloshing action in the pitch plane a r e the vehicle translational acceleration due to thrust in the pitch plane and vehicle attitude acceleration in the pitch plane. These inputs cause the propellants to move against the tank walls which, in turn, causes attitude acceleration to be induced by two factors: the force of the propellant sloshing m a s s acting on tank walls through a moment a r m about the center of gravity, and the sloshing m a s s being displaced from the center line of the vehicle acting through a radial moment a r m about the center of gravity. The model used to simulate the sloshing effect during second and third stages consists of two linear second-order directly coupled differential equations with m a s s varying coefficients. These differential equations describe the radial motion of the slosh m a s s (LOX and LH2) in the pitch plane. H. S-I1 and S-TVB Propellant Utilization Systems (PU) 1. Actual PU System One function of the PU system is to control the LOX and LH2 flow to the thrust chamber in such a manner that depletion of LH2 and LOX will occur simultaneously. Remaining LOX and LH2 a r e measured by capacitance-type probes in each tank. The signal from each probe is gain adjusted so that when the two signals a r e differenced, a resulting signal will drive the PU valve position servo to give a desired EMR. Sloshing (LH2 and LOX) causes the signals representing remaining propellant to vary, which in turn tends to cause the PU valve position, EMR, and thrust to vary at the sloshing (LOX and L H ~ frequencies. ) Since a varying thrust has ill effects on the guidance system, the PU valve control signal is filtered so that sloshing frequencies a r e highly attenuated in the resulting valve control signal. �2. PU Simulation Models Slide 9 depicts a S-IVB PU system model obtained from a MSFC Guidanct This is basically the model used in the Hybrid Dynamics Design Document. Simulation. The S-I1 model is essentially the same except for a different sloshing filter. In the PU model, remaining LH2 and LOX masses at any point in time a r e determined by integrating the total flow r a t e s and subtracting these f r o m the initial LH2 and LOX masses. Slide 9 also shows how the effects of propellant sloshing on the PU system are implemented. VI. COMPUTING TASK ASSIGNMENTS In assigning computing tasks several factors were considered that seemed to fall into two general categories as shown in Slide 10 and as follows: A. Application Orientation 1. Frequency Content In the Hybrid Simulation, models with high frequency content were simulated on the analog computer, which has a bandwidth of several kH. The f r e quency response of digital computers depends on both the algorithms used to represent a given model and the solution r a t e of the algorithms. In general, f o r good accuracy, the solution rate must be several times the highest significant frequency . 2. Precision Requirements Where high precision was required the digital computer was used, because parameter value can be maintained and expressed in much smaller increments. An analog signal value is usually expressed in no more than four o r five decimal places. 3 . System Composition In the r e a l world the LVDC is digital while the FCC is analog. Precision in a simulation need not be greater than it is in the actual system. This was a consideration in assigning the FCC simulation task. MSFC Memo #R-ASTR-F-66-45, Phase I1 Guidance Dynamics Design Document f o r AS-207, 8 March 1966. �Flight Hardware Interface 4. The output of the hardware (LVDC-LVDA) consists of attitude steering commands ( A 4 ) which a r e analog signals. The inputs to the flight hardware a r e platform velocity counts, which a r e discrete in nature, and platform gimbal angles, which a r e analog signals. 5. Type of System One important consideration in some of the model assignments was the time varying coefficients in the differential equations representing the models. The analog computer readily lends itself to modeling the differential equation while the digital computer easily handles time varying coefficients. The models were therefore simulated on a hybrid system using multiplying DAC's to combine the coefficients with the dependent variable and i t s derivatives. B . Simulation Hardware 1. Memory Size and Speed of Digital Computers While memory size can be important, it was not a consideration in this simulation. The speed of the digital computer was a consideration, in that i t determined how fast the various loops in the program could be processed and, therefore, what the solution r a t e s f o r the various model algorithms would be. 2. Equipment Configuration of the Analog Computer Task assignment is largely dependent on the types and number of elements on the analog computer. In this simulation the analog computer specifications were based on the already determined task assignments listed below; thus the elements were not really a consideration in this case. 3 . Linkage Characteristics The bit configuration (word length), conversion rates, and number of channels @/A, A/D, D/D) were important considerations in assigning c e r tain tasks. �4. Communication Channel Count and Precision Versus Consolidation of Small Computing Task on One Machine When implemented all-analog o r all-digital by the use of special techniques, a model which is best suited to hybrid application will use fewer conversion channels but may lose precision and accuracy. C . Assignments Slide 11 shows a list of the actual computing task assignments. a r e as follows: These Analog - - - Flight Control Computer Control Actuator Moment Equations Propellant Slosh Model Body Bending Model Propellant Utilization Control System Digital - - D. Inertial Platform Time and Mass Varying Function Generation Navigation Model Telemetry Ground Station Control of Automated Setup and Checkout of Analog Computer Propellant Utilization System Valve and Pump Model Data Reduction and Preparation Hybrid Simulation Tie -In Tie-in of the total hybrid simulation is presented by tracing system signal flow in the S-IVB stage pitch plane as follows. The analog computer receives the attitude steering command ( A 4 ) from the LVDC-LVDA. The P control computer model filters this signal and sums it with the filtered body attitude rate ($p) generated by the vehicle dynamics model. The resulting signal (PCP)is fed to the actuator model which generates the simulated engine �(9). angle This is then multiplied by the control moment coefficient (CZp), provided by a digital model, to result in a rigid body pitch attitude acceleration due to engine thrust. This component is summed with the attitude acceleration arising from propellant sloshing to give total attitude acceleration ($p). This $p is integrated once to result in rigid body attitude rate (dp)that is summed with attitude rate due to body bending ) to give a simulated body rate gyro bp output (bgp). The propellant sloshing model has a s inputs, engine angle ( 6 ) P and attitude acceleration (Pp), while the bending model is forced by engine angle (Pp) and engine rotational acceleration (b ). P (6 The propellant utilization (PU) system is forced by remaining LOX and LH2 m a s s which a r e computed on a digital computer. The PU system is perturbed by radial positions of propellant sloshing m a s s e s (LOX and LH2). The output of the PU system is valve position (av). A digital computer receives as inputs from the analog models the attitude rate (dgp), the engine angle (Pp), and the PU valve position (8,). The $gp is resolved into the inertial platform frame to result in a platform gimbal angle rate ( 6 p), which is integrated to give the gimbal angle (0 p). The PU valve position (6 ). is used in a table look scheme of total thrust ( F ) versus 6, to obtain F, which is then divided by remaining vehicle m a s s (mv) to result in total vehicle acceleration (F/mv). Vehicle m a s s is computed by subtracting integrated propellant flow rates from initial vehicle mass. Components of body m ~ the engine gimbal angles. acceleration a r e obtained by resolving ~ / through These components a r e in turn resolved through the inertial platform gimbal angles to result in inertial platform accelerations components, which a r e used to compute changes in measured platform velocities. These changes in velocities and the simulated inertial platform gimbal angles a r e transmitted via special interface equipment to the LVDC -LVDA where the accumulated velocity changes a r e used for navigation and computation of commanded platform gimbal angles (x). These x ' s when differenced with the actual platform gimbal angles result in attitude e r r o r signals (+) which a r e transformed into the body frame to result in attitude steering commands (A$). These A $ 's a r e then transmitted t o the analog computer to close the guidance and control loop. �VII. RESULTS In concluding this presentation, some of the results from the AS-204 L M / ~Hybrid Simulation studies will be discussed. Slides 12 and 13 show s t r i p recordings of some of the simulated vehicle and systems dynamics f o r a nominal case. From left to right on Slide 12 a r e the pitch attitude steering command (A$*), pitch engine angles (Bp (1,2) and ($ (3,4), pitch body r a t e (&p), yaw attitude steering command ( ~y), 4 yaw engine angles (fly (2,3) and (Py (1,4), and yaw body rate (&y). Magnitudes of these parameters and significant flight events a r e indicated. Slide 13 shows Cfrom left to right) the roll attitude command @OR), body roll r a t e (eR), radial displacement of the fuel and LOX sloshing m a s s (Z and ZL), remaining LOX and fuel weight (WL and WF), the change in engine mixture ratio (AEMR), and P U valve position (aV). These simulation results compare favorably with actual flight data. All significant differences a r e attributable to uncertainties in certain initial conditions. While results from the hybrid simulation have been good, certain anomalies in actual Saturn flights have revealed a need f o r studies that were not previously considered. These studies can be handled by making slight modifications to certain simulation models. VIII. SUMMARY A hybrid simulation is used to dynamically verify the guidance and cont r o l subsystems of Uprated Saturn I and Saturn V vehicles. This is done by simulating pertinent vehicle dynamics in a closed guidance and flight control loop with flight-type (LVDC and LVDA) hardware in the loop. In conjunction with equipment constraints, the computational complexity imposed by the requirements for high precision solutions of the guidance and navigation equ: throughout the total boost portion of the mission and f o r accurate solution of nonlinear differential equations with variable coefficients and high frequenc: content led to the choice of a hybrid system for this application. This simr has already proven to be a valuable tool fop preflight prediction of vehicle/ system dynamic performance and i t s effects on guidance accuracy. With further developments, it will also be useful for detailed evaluation of dyna. behavior under extreme combinations of off -nominal situations. �LAUNCH ESCAPE SYSTEM LAUNCH ESCAPE SYSTEM COMMAND MODULE SERVICE MODULE COMMAND MODULE SERVICE MODULE ADAPTER S-IVBSTAGE LUNAR LE q+- - - I 1 J -2 ENGINE INSTRUMENT S-IVB STAGE 5-IVB AFT INTERSTAGE --I I . 1 J-2 ENGINE S -IC STAGE S-IB STAGE 8 H-1 ENGINES APOLLO-SATURN V VEHICLE UPRATED SATURN I VEHICLE Slide 1 �SATURN INSTRUMENT UNIT Slide 2 �Instrument Unit Subsystems e STRUC'TURAL PORTION e GU IDANCE AND CONTROL e ENV I RONMENTAL CONTROL e MEAS UR ING AND TELEMETRY e RAD 10 FREQUENCY e ELECTR ICAL Slide 3 15 �Guidance and Control Subsystem o LAUNCH VEHICLE DIGITAL COMPUTER (LVDC) o LAUNCH VEHICLE DATA ADAPTER (LVDA) o FLIGHT CONTROL COMPUTER (FCC o ST 124 INERTIAL PLATFORM a BODY RATE GYROS Slide 4 16 �Simplified Saturn V Slide 5 17 �Guidance and Control System - .. .. .. Xm ' Ym ' Zm lnertial Platform Assernbl y >P ------------------- B~ - I I I -% JJ I I inertial Velocities (~11,A V , OW) Inertial Platform Gimbal Angles ( 0 ) 1 __c LVDC -1 -1 LVDA n v ~ b Flight Control Computer @CP Engine Actuator Vehicle . -@% Dynamics I A A ' -vT' ' PU System Rate Gyro --------- Slide 6 18 I I I �FLIGHT COMPUTER TASKS B Y PHASE 185 Kilometers (100 Naut. Miles I SATURN V I APOLLO PHASE t Slide 7 19 I TASK I �Control Loop Slide 8 �Propellant Utilization System z~ ,c o s e F SLOSH INITIAL L H 2 ~ t ~LH2~ ~ ~ -- . 8wF a z ~ FROM SLOSH MODEL NOMINAL L H ~ FLOW RATE I LH2 BRIDGE SERVO I 'PU K~ ( d s 2 cs5 t 6s4 - - bS ' - es3 fs2 g s POSlTlONER VALVE AA\P FORWARD SHAPING -1 VALVE : K~ I GEARS & POT REDBACK I LOX BRIDGE SERVO - - 2C~"~ , 1 1\ .s K~~ z~ FROM SLOSH MODEL - ' coseL . IINITIAL aW~ aZL LOX SLOSH WEIGHT Slide 9 LOX WEIGHT I N O M l NAL LOX FLOW RATE Lox TO THRUST MODEL �Factors Related to Computing Task Assignments in Hybrid Simulation 1. APPLICATION a. b. c. d. e. 2. FREQUENCY CONTENT PREC IS ION REQU I REMENTS SYSTEM COMPOS IT1ON FLIGHTEQUIPMENT INTERFACE TYPE OF SYSTEM COMPUTER HARDWARE a. b. c. d. MEMORY S I Z E AND SPEED OF D I G l T A L MEMBER EQU I PMENT CONFIGURATION OF ANALOG MEMBER LINKAGE CHARACTER1 STICS COMMUNICATION CHANNEL COUNT AND PRECISION vS CONSOLIDATION OF SMALL COMPUTING TASK ON ONE MACHINE Slide 10 22 �Computing Task Assignment ANALOG a a a a a a FLIGHT CONTROL COMPUTER CONTROL ACTUATOR MOMENT EQUATIONS PROPELLANT SLOSH MODEL BODYBENDINGMODEL PROPELLANT UTl L l ZATl ON CONTROL SYSTEM DIGITAL a a a a a 0 0 lNERTl AL PLATFORM TIME ANDIOR MASS VARYING FUNCTIONS GENERATION NAVIGATION MODEL TELEMETRY GROUND STATION CONTROL OF AUTOMATED SET-UP AND CHECKOUT OF ANALOG PROPELLANT UTILIZATION SYSTEM VALVE AND PUMP MODELS DATA REDUCTION AND PREPARATION Slide 11 23 �Slide 12 �Slide 13 �4 Federal Systems Division, Space Systems Center, ~untsville,Alabama � 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_000055 Title A name given to the resource "A Hybrid Simulation for Dynamic Verification of Saturn Guidance and Control Subsystems." Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. IBM No. 68-U60-0013 Description An account of the resource This paper presents a discussion of a hybrid simulation used to dynamically verify the Saturn Guidance and Control subsystems. First, the Saturn vehicle is briefly described to provide background information. The Instrument Unit (IU) is considered in more detail to give a proper setting for the Guidance and Flight Control (G and FC) discussion that follows. After a brief description of the actual G and FC System operation, simulation models of the G and FC components are considered in detail. This is followed by a discussion of the model assignment to a particular computer (digital or analog) and justification for making that assignment. Finally, results of the AS-204/LM1 hybrid simulation studies are briefly considered with mention of the actual flight data. Creator An entity primarily responsible for making the resource Patray, Ronald T. International Business Machines Corporation. Federal Systems Division Date A point or period of time associated with an event in the lifecycle of the resource 1965-07 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn Project (U.S.) Project Apollo (U.S.) Saturn launch vehicles Apollo spacecraft Spacecraft guidance Spacecraft control Computerized simulation Dynamic tests 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 26, Folder 34 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/207/14696/The_Montgomery_Advertiser_1989_10_21_14_photos.jpg c0ae555d4950847a4db3d3604fb57d2e 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_Montgomery_Advertiser_1989_10_21_14_photos Title A name given to the resource Montgomery Advertiser Photographs of AIDS Outreach Description An account of the resource A clipping of the digitization of the October 21, 1989 edition of the Montgomery Advertiser's Religion Section that has a photograph of AIDS outreach attempts by churches. The top photo is of Revs. Elizabeth Leech (left) and Stephen Pieters. The bottom photo is of Rev. William Rupracht. Creator An entity primarily responsible for making the resource Patricia Miklik Jamie Sturtevant Publisher An entity responsible for making the resource available Montgomery advertiser Date A point or period of time associated with an event in the lifecycle of the resource 1989-10-21 Temporal Coverage Temporal characteristics of the resource. 1980-1989 Spatial Coverage Spatial characteristics of the resource. Alabama Montgomery (Ala.) Subject The topic of the resource AIDS (Disease) AIDS (Disease) in mass media AIDS (Disease)--History AIDS (Disease)--Religious aspects Type The nature or genre of the resource Newspapers Clippings Source A related resource from which the described resource is derived The Montgomery Advertiser, Newspapers.com, Ancestry.com (LLC) https://www.newspapers.com/image/258027054/ 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/33/4698/loc_gold_000292_000292.pdf b686643aea888967f18580bf9a509fe5 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 Goldsmith-Schiffman Collection Identifier An unambiguous reference to the resource within a given context Goldsmith-Schiffman Collection Description An account of the resource <p>"My ancestors were all German Jewish immigrants, members of four families who settled in Huntsville, Alabama before and following the Civil War. The Bernstein, Herstein and Schiffman families arrived during the 1850s, and Oscar Goldsmith arrived in 1879. Subsequent generations united these four families in marriage. Members of the extended family have figured in every phase of the history of Huntsville, both economically and socially; from the agrarian years of the nineteenth century through Huntsville’s growth after World War II, to becoming known as Rocket City USA; and socially, from the time of institutionalized slavery before the Civil War to segregation followed by the civil rights era."</p> <p>-<a href="https://www.myjewishlearning.com/southern-and-jewish/highlighting-the-history-of-huntsvilles-jewish-community/">Margaret Anne Goldsmith in an interview with My Jewish Learning</a></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 loc_gold_000292_000292 Title A name given to the resource Receipt for Oscar Goldsmith payment to Leo N. Levi Memorial Hospital. Description An account of the resource Receipt for Oscar Goldsmith's payment of five dollars to Leo N. Levi Memorial Hospital. The hospital is located in Hot Springs, Arkansas and is a mental health facility and, at this time, a nursing school that existed until 1952. Creator An entity primarily responsible for making the resource Patterson, Susan Date A point or period of time associated with an event in the lifecycle of the resource 1923-01-18 Temporal Coverage Temporal characteristics of the resource. 1920-1929 Subject The topic of the resource Hospital benefactors Mental health services Nursing schools Payment Hot Springs (Ark.) Huntsville (Ala.) Madison County (Ala.) Type The nature or genre of the resource Receipts (financial records) Text Source A related resource from which the described resource is derived I. Schiffman and Company Box 99, Folder Misc. Correspondence 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_gold_2021_02 https://digitalprojects.uah.edu/files/original/108/7045/r01b01-05.pdf caa2fe8888052769a6107e66eff63130 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 01, Subseries B: Cabaniss Professional Business Title A name given to the resource Series 01, Subseries B: Cabaniss Professional Business Description An account of the resource Sub series B (CPB) deals with a small, but active, legal practice of Septimus Cabaniss with his various partners, who included men considered to be outstanding lawyers in the state, from the 1890s to 1938 at the office on the town Square. He studied law in Huntsville under Silas Parsons and practiced law with Leroy Pope Walker, Robert C. Brickell, and Francis P. Ward. These papers are sorted by year, except when an obvious grouping of an estate is evident. The papers continue through professional activities at the Madison County Courthouse including those of his son, James Budd Cabaniss, and his daughter, Fanny Cabaniss, who were clerks of the Chancery Court and a few papers of his son, Septimus, Jr., who owned a bookstore for a brief period. 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 r01b01-05 Title A name given to the resource Legal and court documents, 1830s Relation A related resource r01b-210907 Creator An entity primarily responsible for making the resource Patton & Donnegan Co. Greene, H. Boardman, John McClung, James Henderson, Richard Temporal Coverage Temporal characteristics of the resource. 1830-1839 Subject The topic of the resource Courtland (Ala.) Guano industry Ledgers Enslavement Limestone County (Ala.) Type The nature or genre of the resource Correspondence Legal documents 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. Source A related resource from which the described resource is derived Frances C. Roberts Collection, Series 1, Subseries B, Box 1, Folder 5, University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/108/7040/r01b01-10.pdf 28a700e4922d332c77ba2b917abc219f 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 01, Subseries B: Cabaniss Professional Business Title A name given to the resource Series 01, Subseries B: Cabaniss Professional Business Description An account of the resource Sub series B (CPB) deals with a small, but active, legal practice of Septimus Cabaniss with his various partners, who included men considered to be outstanding lawyers in the state, from the 1890s to 1938 at the office on the town Square. He studied law in Huntsville under Silas Parsons and practiced law with Leroy Pope Walker, Robert C. Brickell, and Francis P. Ward. These papers are sorted by year, except when an obvious grouping of an estate is evident. The papers continue through professional activities at the Madison County Courthouse including those of his son, James Budd Cabaniss, and his daughter, Fanny Cabaniss, who were clerks of the Chancery Court and a few papers of his son, Septimus, Jr., who owned a bookstore for a brief period. 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 r01b01-10 Title A name given to the resource Legal and court documents, 1845 Relation A related resource r01b-210907 Creator An entity primarily responsible for making the resource Patton, W.R. Fearn, Thomas Subject The topic of the resource Calico Presbyterian Church Talladega County (Ala.) Banks and banking Cotton trade Type The nature or genre of the resource Memorandum Correspondence Deeds 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. Temporal Coverage Temporal characteristics of the resource. 1840-1849 Source A related resource from which the described resource is derived Frances C. Roberts Collection, Series 1, Subseries B, Box 1, Folder 10, University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama https://digitalprojects.uah.edu/files/original/20/2340/spc_stnv_000112.pdf d4c88127fd9a2484ec76db78592484d6 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_000112 Title A name given to the resource "A Review of Cryogenic Technology Aspects of Space Flight." Description An account of the resource This paper was presented at the International Cryogenic Engineering Conference in Kyoto, Japan. It details the use of cryogenic technology in rocketry and how its usage created "many new techniques and deeply stimulated many fields of cryogenic technology." Creator An entity primarily responsible for making the resource Paul, H. G. Wood, Charles C. Date A point or period of time associated with an event in the lifecycle of the resource 1967-04 Subject The topic of the resource Cryogenic rocket propellants Liquid propellant rocket engines Liquid propellant rockets--Fuel systems Liquid propellants Low temperature engineering Saturn Project (U.S.) Source A related resource from which the described resource is derived Saturn V Collection Box 22, Folder 3 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_000075_000118 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="%E2%80%9Dhttp%3A//libarchstor.uah.edu:8081/repositories/2/archival_objects/17663%E2%80%9D">View this item in ArchivesSpace</a> Temporal Coverage Temporal characteristics of the resource. 1960-1969 Type The nature or genre of the resource Reports Still image Text https://digitalprojects.uah.edu/files/original/20/11021/DigeofFY-64fundadvastudaugu1966_110707112556.pdf af38a78d58cf33f3ec1bd9625917cb40 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 DigeofFY-64fundadvastudaugu1966.pdf spc_stnv_000250 Title A name given to the resource "Digest of FY-64 Funded Advanced Studies: August 1966." Description An account of the resource This paper outlines the major advantages of digital transducers and describes the principles and features (1) direct digital transducers, (2) indirect digital transducers, (3) quasi-digital transducers, and (4) A to D transducers. The mutual effect of transducers and systems will be discussed briefly, and some trends of transducer research and development will be presented. Creator An entity primarily responsible for making the resource Payne, William R. George C. Marshall Space Flight Center. Research Program Office Date A point or period of time associated with an event in the lifecycle of the resource 1966-08-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Astronautics Type The nature or genre of the resource Text Essays Source A related resource from which the described resource is derived Saturn V Collection Box 18, Folder 19 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_000250_000274 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17513"> View this item in ArchivesSpace</a> https://digitalprojects.uah.edu/files/original/20/11023/digoffy65funadvstujul1966_090707104031.pdf cd19dca91881f3c56fe562d4df53bfba 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 digoffy65funadvstujul1966_090707104031.pdf spc_stnv_000252 Title A name given to the resource "Digest of FY-65 Funded Advanced Studies:July 1966." Description An account of the resource This publication is one of a planned series to summarize the advanced study program for each fiscal year beginning with FY-61.A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide reference information which should be helpful in planning future study programs. The FY-65 funded studies are covered in this document. These investigations are covered under four major headings: Launch Vehicle Studies, Earth Orbital and Lunar Studies, Planetary/Nuclear Studies, and AAP Studies. The information presented on each studyincludes a brief description of the objectives and pertinent contract data. Creator An entity primarily responsible for making the resource Payne, William R. George C. Marshall Space Flight Center. Research Program Office Date A point or period of time associated with an event in the lifecycle of the resource 1966-07-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Astronautics Type The nature or genre of the resource Text Summaries Source A related resource from which the described resource is derived Saturn V Collection Box 17, Folder 65 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_000250_000274 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17488"> View this item in ArchivesSpace</a> https://digitalprojects.uah.edu/files/original/20/11024/digoffy66funadvstunov1966_121407110639.pdf 1c6cc1d69e8f580264b0c7d312cca555 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 digoffy66funadvstunov1966.pdf spc_stnv_000253 Title A name given to the resource "Digest of FY-66 Funded Advanced Studies: November 1966." Description An account of the resource This publication is one of a planned series to summarize the advanced study program for each fiscal year beginning with FY-61.A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide reference information which should be helpful in planning future study programs. The FY-65 funded studies are covered in this document. These investigations are covered under four major headings: Launch Vehicle Studies, Earth Orbital and Lunar Studies, Planetary/Nuclear Studies, and AAP Studies. The information presented on each studyincludes a brief description of the objectives and pertinent contract data. Creator An entity primarily responsible for making the resource Payne, William R. George C. Marshall Space Flight Center. Research Program Office Date A point or period of time associated with an event in the lifecycle of the resource 1966-11-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Astronautics Type The nature or genre of the resource Text Summaries Source A related resource from which the described resource is derived Saturn V Collection Box 19, Folder 32 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_000250_000274 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17553"> View this item in ArchivesSpace</a> https://digitalprojects.uah.edu/files/original/20/11062/Digefy62fund_101507152813.pdf 4cd202eab52449b1306a533daebd7e2b 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 Digefy62fund_101507152813.pdf spc_stnv_000248 Title A name given to the resource "Digest of FY-62 Funded Advanced Studies : July 1966." Description An account of the resource This publication is one of a planned series to summarize the MSFC advanced study program for each fiscal year beginning with FY-61. A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide historical reference information which should be helpful in planning future study programs. The FY-62 funded studies are covered in this document. These investigations are covered under two major categories: Launch Vehicle Studies; and Lunar, Orbital, and Planetary Studies. The information presented on each study includes a brief description of the objectives and results and pertinent contract data. In order to keep this report small and easy to use, no attempt was made to include conclusions based on the study results ; however,the final reports documenting the investigations are referenced. If these reports are needed for permanent retention and are not available from the MSFC Library (MS-IPL), submit requests for the documents to the Scientific and Technical Information Facility, Attention: NASA Representative, P.0. Box 33, College Park, Maryland 20740. Creator An entity primarily responsible for making the resource Payne, William R. Date A point or period of time associated with an event in the lifecycle of the resource 1966-07-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Astronautics--United States George C. Marshall Space Flight Center. Research Program Office Type The nature or genre of the resource Text Essay Source A related resource from which the described resource is derived Saturn V Collection Box 17, Folder 71 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_000225_000249 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17494"> View this item in ArchivesSpace </a> https://digitalprojects.uah.edu/files/original/20/11063/Digefy62fund_101507152239.pdf 51d13124acf8e1821a8cd664453cd4dd 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 Digefy62fund_101507152239.pdf spc_stnv_000249 Title A name given to the resource "Digest of FY-63 funded advanced studies : July 1966." Description An account of the resource This publication is, one of a planned series to summarize the advanced study program for each fiscal year beginning with FY-61. A separate report will cover the study program for each fiscal year. The purpose of these documents is to provide historical reference information which should be helpful in planning future study programs. The FY-63 funded studies are covered in this document. These investigations are covered under three categories: Launch Vehicle and Supporting Studies; Orbital and Lunar Studies; and Planetary Studies. The information presented on each study includes a brief description of the objective and results and pertinent contract data. In order to keep this report small and easy to use, no attempt was made to include conclusions based on the study results; however, the final reports documenting the investigations are referenced. If these reports are needed for permanent retention and are not available from the Technical Supervisor or the MSFC Library (MS-IPL), submit requests for the documents to the Scientific and Technical Information Facility, Attention: NASA Representative, P. O. Box 33, College Park, Maryland 20740. Creator An entity primarily responsible for making the resource Payne, William R. Date A point or period of time associated with an event in the lifecycle of the resource 1966-07-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn project Astronautics--United States George C. Marshall Space Flight Center. Research Program Office Type The nature or genre of the resource Text Essay Source A related resource from which the described resource is derived Saturn V Collection Box 17, 72 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_000225_000249 Is Referenced By A related resource that references, cites, or otherwise points to the described resource. <a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17495"> View this item in ArchivesSpace </a> https://digitalprojects.uah.edu/files/original/20/1280/spc_stnv_000138.pdf c9bb3a070ddfa814f788381bfa212c11 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_000138 Title A name given to the resource "Bibliography of Research and Development Reports on the Centaur Program for Period 1958-1962." Alternative Title An alternative name for the resource. The distinction between titles and alternative titles is application-specific. GDA-AOC63-0400 Description An account of the resource Contract AF 18(600)-1775AD 815-832. Original is 6 sheets of microforms. Pages i, ii, iv, vi-xii, 110 and 344 missing on microforms. The title page notes that the document "Supersedes AE62-0400 and Supplements -A, -B, &amp; -C." Creator An entity primarily responsible for making the resource Peck, T. P. General Dynamics Corporation Date A point or period of time associated with an event in the lifecycle of the resource 1963-03-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Centaur launch vehicle Centaur project Government contractors--United States Research and development Type The nature or genre of the resource Bibliographies Text Source A related resource from which the described resource is derived Saturn V Collection Box 8, Folder 15 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/17312 https://digitalprojects.uah.edu/files/original/75/1561/spc_spac_000306_000309.pdf ea13972e6dbc84b2c9aad9881dee42c6 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 Space City Collection Title A name given to the resource Space City Collection Description An account of the resource Space City was to be an outer space theme park fantasy based in Huntsville; it was to capitalize on space's growing popularity as putting man on the moon became closer and closer to reality. The park's construction began in January 1964. Though a popular idea with the residents, the park ran into various difficulties and was never opened to the public or even fully completed. Construction was abandoned, and the land was put up for auction on October 17, 1967. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/166">View the Space City Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_spac_000306_000309 Title A name given to the resource "The Trackless/Train-Of Penn Ridge Products." Description An account of the resource This leaflet contains photographs, descriptions, and specifications of the Trackless/Train. Creator An entity primarily responsible for making the resource Penn Ridge Products Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Amusement parks--Planning Amusement rides Motor vehicles Type The nature or genre of the resource Leaflets Still Image Text Source A related resource from which the described resource is derived Space City Collection Box 3 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_spac_2020_02 Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection was generously loaned for digitization by Dustin Shannon. The collection is digital only. https://digitalprojects.uah.edu/files/original/204/14609/Natioanl_Cyclists_Union_Record_Letter_1892.pdf c26e813ea905877ee193ce45376aa561 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 HON 399 Research in London Title A name given to the resource HON 399 Research in London 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 Letter from National Cyclists' Union with Shoreland's Record The Cuca Cup Race - Wheeling Description An account of the resource One of the sources on this document is a letter from the National Cyclists' Union addressed to Frank Shorland to recognize him for his 24 hour safety bicycle record. An excerpt from Wheeling magazine about the first edition of the Cuca Cup Race. This source describes the starters, race, and final results. Creator An entity primarily responsible for making the resource Percy A. Nix, Secretary of Records Committee Publisher An entity responsible for making the resource available Wheeling Date A point or period of time associated with an event in the lifecycle of the resource 1892-8-12 1892-7-27 Subject The topic of the resource Cycling Record Source A related resource from which the described resource is derived University of Warwick, Modern Records Centre, National Cycle Archive Is Part Of A related resource in which the described resource is physically or logically included. "Herne Hill Velodrome and the Cuca Cocoa Challenge Cup", by Colby Winters, HON 399 Research in London, Spring 2024 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. HON 399 Honors College Student Projects Study Abroad https://digitalprojects.uah.edu/files/original/75/1549/spc_spac_000285_000286.pdf af5423fc24081ece73a3a012c709e588 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 Space City Collection Title A name given to the resource Space City Collection Description An account of the resource Space City was to be an outer space theme park fantasy based in Huntsville; it was to capitalize on space's growing popularity as putting man on the moon became closer and closer to reality. The park's construction began in January 1964. Though a popular idea with the residents, the park ran into various difficulties and was never opened to the public or even fully completed. Construction was abandoned, and the land was put up for auction on October 17, 1967. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/166">View the Space City Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_spac_000285_000286 Title A name given to the resource "Super-Kompak Coinpassor." Description An account of the resource This advertisement provides images, features, models, and specifications for the "Modern, Coin Controlled Turnstile." Creator An entity primarily responsible for making the resource Perey Turnstile Company Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Amusement parks--Equipment and supplies Type The nature or genre of the resource Advertisements Fliers (Printed matter) Still Image Text Source A related resource from which the described resource is derived Space City Collection Box 3 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_spac_2020_02 Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection was generously loaned for digitization by Dustin Shannon. The collection is digital only. https://digitalprojects.uah.edu/files/original/75/1550/spc_spac_000287_000288.pdf 6b04aa44ba8c62efd9742a6676bbd94c 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 Space City Collection Title A name given to the resource Space City Collection Description An account of the resource Space City was to be an outer space theme park fantasy based in Huntsville; it was to capitalize on space's growing popularity as putting man on the moon became closer and closer to reality. The park's construction began in January 1964. Though a popular idea with the residents, the park ran into various difficulties and was never opened to the public or even fully completed. Construction was abandoned, and the land was put up for auction on October 17, 1967. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/166">View the Space City Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_spac_000287_000288 Title A name given to the resource "No. 20-Deep Arm-Traffic Controller." Description An account of the resource This advertisement provides images, features, specifications, and installation diagrams for the "All Metal, One Way, Non-Registering Turnstile." Creator An entity primarily responsible for making the resource Perey Turnstile Company Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Amusement parks--Equipment and supplies Type The nature or genre of the resource Advertisements Fliers (Printed matter) Still Image Text Source A related resource from which the described resource is derived Space City Collection Box 3 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_spac_2020_02 Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection was generously loaned for digitization by Dustin Shannon. The collection is digital only. https://digitalprojects.uah.edu/files/original/75/1551/spc_spac_000289_000292.pdf 56740e63f71a2a04fa5e34089007da6c 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 Space City Collection Title A name given to the resource Space City Collection Description An account of the resource Space City was to be an outer space theme park fantasy based in Huntsville; it was to capitalize on space's growing popularity as putting man on the moon became closer and closer to reality. The park's construction began in January 1964. Though a popular idea with the residents, the park ran into various difficulties and was never opened to the public or even fully completed. Construction was abandoned, and the land was put up for auction on October 17, 1967. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/166">View the Space City Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_spac_000289_000292 Title A name given to the resource "Kompak Coinpassor Model 97." Description An account of the resource This advertisement provides images, features, and specifications for the turnstile. Creator An entity primarily responsible for making the resource Perey Turnstile Company Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Amusement parks--Equipment and supplies Type The nature or genre of the resource Advertisements Fliers (Printed matter) Still Image Text Source A related resource from which the described resource is derived Space City Collection Box 3 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_spac_2020_02 Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection was generously loaned for digitization by Dustin Shannon. The collection is digital only. https://digitalprojects.uah.edu/files/original/75/1552/spc_spac_000293_000294.pdf 668e77db902fae3666b301dc752f4f42 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 Space City Collection Title A name given to the resource Space City Collection Description An account of the resource Space City was to be an outer space theme park fantasy based in Huntsville; it was to capitalize on space's growing popularity as putting man on the moon became closer and closer to reality. The park's construction began in January 1964. Though a popular idea with the residents, the park ran into various difficulties and was never opened to the public or even fully completed. Construction was abandoned, and the land was put up for auction on October 17, 1967. Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/166">View the Space City Collection finding aid on ArchivesSpace</a> Dublin Core The Dublin Core metadata element set is common to all Omeka records, including items, files, and collections. For more information see, http://dublincore.org/documents/dces/. Identifier An unambiguous reference to the resource within a given context spc_spac_000293_000294 Title A name given to the resource "Ful-Stride Roto-Gate." Description An account of the resource This advertisement provides images, features, and specifications for the "Type B Impenetrable" gate. The back of the flier has two illustrations, one of children being prevented from sneaking into the park, and one focusing on the ease of the gate's use. Creator An entity primarily responsible for making the resource Perey Turnstile Company Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Amusement parks--Equipment and supplies Type The nature or genre of the resource Advertisements Fliers (Printed matter) Still Image Text Source A related resource from which the described resource is derived Space City Collection Box 3 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_spac_2020_02 Provenance A statement of any changes in ownership and custody of the resource since its creation that are significant for its authenticity, integrity, and interpretation. The statement may include a description of any changes successive custodians made to the resource. This collection was generously loaned for digitization by Dustin Shannon. The collection is digital only. https://digitalprojects.uah.edu/files/original/20/1666/chemspaceboosters_041807125251.pdf 042071eb3a8465eb77771613eda3d186 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 chemspaceboosters.pdf spc_stnv_000193 Title A name given to the resource "Chemistry in Space Boosters" presentation given at Huntsville High School. Description An account of the resource The document is a draft of the presentation "Chemistry in Space" by Harold Perkins, who explains the role of chemists in developing space launch vehicles. The document Includes references to charts and other presentation supports. The document is marked in the upper left hand corner "Huntsville High School Science Organization (the JETS), October 1962." Creator An entity primarily responsible for making the resource Perkins, Harold Date A point or period of time associated with an event in the lifecycle of the resource 1962-10-01 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Saturn 5 stage Saturn Project (U.S.) Space vehicles--Propulsion systems Booster rocket engines Chemistry Huntsville City Schools (Huntsville, Ala.) Huntsville (Ala.) Madison County (Ala.) Source A related resource from which the described resource is derived Saturn V Collection Box 7, Folder 32 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_000175_000199 Type The nature or genre of the resource Speeches Transcripts Text https://digitalprojects.uah.edu/files/original/57/2696/spc_mcca_000394-397.pdf 7ee1442ceafa487be59a3d4d688df102 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 Christel W. Ludewig McCanless Collection Title A name given to the resource Christel W. Ludewig McCanless Collection Relation A related resource <a href="http://libarchstor.uah.edu:8081/repositories/2/resources/17" target="_blank" rel="noreferrer noopener">View the Christel W. Ludewig McCanless Collection finding aid in ArchivesSpace</a> Description An account of the resource Christel Ludewig McCanless was born in Germany in 1939. Her father, Hermann Ludewig, was one of the V-2 engineers at Peenemuende. Consequently, she grew up in Peenemuende until an air raid in 1943 destroyed their home. McCanless and her family moved to Trebbin, Germany, which became part of East Germany after World War II. In 1953, Ludewig accepted a job to work with Von Braun in Huntsville, Alabama and decided to flee East Germany with his family. McCanless continued school in the United States and graduated with a Bachelor of Arts in English from the University of Montevallo and then graduated with a Masters in Library Science from the University of North Carolina at Chapel Hill. She served as the first full-time, professional librarian at UAH. After serving as the Library Director at UAH, she worked in the Huntsville Times newspaper library, the Huntsville Museum of Art’s Art Reference Library, and the Huntsville Museum of Art’s Education Resource Center. In addition, she consulted for the Alabama Library Exchange and created workshops on technology and library science. McCanless is the author of "Fabergé and His Works: An Annotated Bibliography of the First Century of His Art" and a co-author of "Fabergé Eggs: A Retrospective." 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_mcca_000394_000397 Title A name given to the resource Memorandum from Jean Perrault to the UAH faculty concerning the request of books and journals. Description An account of the resource This memorandum describes the changes in the process of requesting materials for the library to purchase. These changes include a new requirement for a value judgement of the requested material when filling out a request slip. Attached is a chart that displays the selection and maintenance process for new materials. Creator An entity primarily responsible for making the resource Perrault, Jean Michel Date A point or period of time associated with an event in the lifecycle of the resource 1968-08 Temporal Coverage Temporal characteristics of the resource. 1960-1969 Subject The topic of the resource Academic libraries Library administration Universities and colleges—Faculty University of Alabama in Huntsville 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 Christel L. McCanless Collection Box 1, Folder 56 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_mcca_2020_11