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Marshall Space Flight Center Space Day 1961 program.
The program includes "Marshall Center Highlights" from the Center's first year, a message from director Wernher von Braun, a photograph of the Space Queen and Princesses, and a guide to the Center's buildings. -
"Saturn and Noise."
The pamphlet uses a cartoon character named "D. B. Noyes" to explain to the public "the nature and effects of the noise which Saturn makes during static firing tests." -
"Saturn V Apollo Flight Configuration."
Drawn by Don Sprague at the Huntsville Engineering section of Boeing. -
Saturn V history team at the Apollo 10 launch.
Shown left to right: David Christensen, Melvin Kranzberg, Irving B. Holley, Jr., Rudolf Hermann, and Fred Ordway. -
"A Hybrid Simulation for Dynamic Verification of Saturn Guidance and Control Subsystems."
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. -
"Saturn Radar Altimeter."
Paper given at the AIAA Guidance and Control Conference, August 12-14, 1963, Massachusetts Institute of Technology, Cambridge, Massachusetts. -
"All Digital Simulation of Saturn I, IB, and V: Boost Vehicle and Guidance Control Systems."
The introduction notes, "The Saturn V launch vehicle is being developed by the National Aeronautics and Space Administration's George C. Marshall Space Flight Center for Project Apollo; Saturn I and Saturn IB vehicles are providing the early testing and support for Project Apollo. The nerve center of the Saturn is its guidance and control system. An airborne digital computer provides the link which closes both the guidance and control loops,making verification of the flight computer program of vital importance. During a powered flight this onboard digital computer program can be divided into four major parts:a) guidance, including navigation, b) control, c) vehicle sequencing, and d) computer telemetry." -
"Analog Simulation of Saturn S-IB Stage Propulsion System Dynamic Characteristics."
This copy has handwritten notes that change the title to read, "Analog Simulation of Uprated Saturn I Stage Propulsion System Dynamic Characteristics." The abstract notes, "The purpose of this paper is to present the techniques and logic employed in the development of an analog computer model to simulate Saturn IV first stage propulsion system dynamic characteristics. Restraints, problem areas, and major assumptions are included." -
"Saturn V First Stage Annual Progress Report: Fiscal Year 1968."
The report covers June 30, 1967 through June 27, 1968: Contract NAS8-5608, Schedules 1 and 1A, July 27, 1968. Prepared by J. P. Delaloye, Management Reporting and Analysis; Supervised by D. G. Valentine, Management Reporting and Analysis; Approved by R. F. Terry, Program Reports; D. H. Creim, Michoud, Program Planning and Reporting Manager; E. K. Cooper, S-IC Program Executive. -
Apollo 10/AS-505 mission chart.
The chart includes diagrams, mission statistics, crew, and notes. There is an additional copy in the David Christensen Collection. -
Apollo 10 press kit.
The press kit includes documentation on the Command and Service Module, Lunar Module, Saturn V launch vehicle, astronauts, and mission descriptions. Release No. 69-68. -
Final Apollo 11 Lunar Surface Operations Plan.
Prepared by the Lunar Surface Operations Office, Mission Operations Branch, Flight Crew Support Division. -
"Apollo 6 Pre-Launch Press Conference."
The press conference was given at Cape Royal News Center in Cocoa Beach, Florida, on Wednesday, April 3, 1968, at 3:30 PM. Participants: William C. Schneider, Apollo Mission Director, NASA; George M. Low, Apollo Spacecraft Manager, NASA; Clifford Charlesworth, Apollo 6 Flight Director, Manned Spacecraft Center, NASA; Dr. Arthur Rudolph, Saturn V Program Office, Marshall Space Flight Center, NASA; Rocco A. Petrone, Apollo 6 Launch Director, Kennedy Space Center, NASA; Col. Royce Olson, USAF, Director DOD Manned Spaceflight Support Office, Patrick AFB; Chris Kraft, Director of Flight Operations, Manned Spacecraft Center. -
"Assurance and Measurement of Space Vehicle Alignment."
Prepared by A. W. Dryden, Quality Engineer, Quality Engineering, Reliability Assurance, Space Systems Center, Douglas Aircraft Company, Inc., Huntington Beach, California. Presented to the 21st Annual Technical Conference for the American Society for Quality Control, Chicago, Illinois. 30 May to 2 June 1967. -
Saturn Launch Vehicles Astrionics System Handbook, 2nd revised edition.
This updated edition of the Astrionics System Handbook instructs, "The enclosed pages change, delete, or supplement the information in the Astrionics System Handbook (1 August 1965). Insert these pages and destroy the pages they replace." -
Saturn Launch Vehicles Astrionics System Handbook.
Includes change pages. Contract NAS8-14000. Second revised edition. V66-15610. NASA-CR71607. The introduction notes, "This second revised edition of the Astrionics System Handbook has been developed under the direction and overall supervision of Dr. Rudolf Decher of the Astrionics Systems Engineering Office. This description of the Saturn Astrionics System has been generated by personnel of the Astrionics Laboratory, the staff of the Astrionics Systems Engineering Office, and by personnel of the International Business Machines Corporation working under Contract NAS8- 14000. The handbook will be updated and expanded as it becomes necessary due to changes or refinements in the system concept and hardware. Sections not contained in the first release of this document will be made available within three months." Signed by Ludie G. Richard, Chief, Systems Engineering Office, Astrionics Laboratory. The document is missing pages in the following locations: Chapters 8, 9, 12. Sections 15.2, 15.3, 15.4-1 thru 15.4-16, 15.5-1 thru 15.5-2, 15.5-5 thru 15.5-8. -
"Automatic Saturn V Page Test System."
The abstract notes, "This paper describes the Automatic Saturn V Page Test System. The system is used to evaluate microminiature Unit Logic Device (ULD) circuits. A page is an assembly consisting of a magnesium- lithium frame, an input-output connector, test points, and multilateral printed circuit boards that interconnect the IUDs into logic circuits. The test system automatically performs tests for shorted voltages and shorted diodes, static logic function, and pulse function."