Title
Select... "1965 Publications," Materials Division, George C. Marshall Space Flight Center. "A 'Zero Stage' for the Saturn IB Launch Vehicle." "A Bibliography of Wernher von Braun, 1965." "A Bibliography of Wernher von Braun, 1967." "A Bibliography of Wernher von Braun." "A Comparison of Advanced Cooling Techniques for Rocket Thrust Chambers". "A comparison of four control systems proposed for Saturn V launch vehicles." "A decade of space progress, 1958 to 1968: General Electric Missile and Space Division offers a pictorial tribute to the National Aeronautics and Space Administration." "A Description of the ST 124-M Inertial Stabilized Platform and its Application to the Saturn V Launch Vehicle." "A description of the ST-124M inertial stabilized platform and its application to the Saturn V launch vehicle." "A Discussion of the Lunar Landing Problem." "A Helium Face Seal Application In a Liquid Oxygen Pump." "A Hybrid Simulation for Dynamic Verification of Saturn Guidance and Control Subsystems." "A Nation Goes to the Moon." "A new telemetry technique." "A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads." "A Prime Contractor's Reliability Program for Components/Parts for the Douglas S-IVB Stage Project." "A Program plan for earth orbital space astronomy." "A real time operating system for the Saturn V launch computer system." "A Review of Cryogenic Technology Aspects of Space Flight." "A review of the research origins of the LANCE weapon system -- Project hindsight -- Task 1 supplement." "A Second Look at Man, Machine, and Automatic Test Operations." "A Study of Saturn V and Intermediate Vehicle Improvement Programs Executive Summary Report." "A summary of major NASA launchings" between October 1st and December 31st, 1968. "A survey of propulsion problems as related to space vehicle design." "AAP review slated next week." "Administrator's Statement on the Selection of a Contractor for the Saturn S-IV Stage." "Advances in Pumping Technology and Rocket Engine Turbopump Applications." "Aero-Astrodynamics Laboratory bimonthly progress report : August and September 1967." "Aero-Astrodynamics Laboratory Bimonthly Progress Report, April and May 1967." "Aero-Astrodynamics Laboratory Bimonthly Progress Report, December 1967-January 1968." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: April - May 1968." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: December 12, 1966." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: December 13, 1965." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: December 1968 - January 1969." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: February - March 1967." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: February - March 1968." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: June - July 1967." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: June - July 1968." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: November 2, 1965." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: October - November 1968." "Aero-Astrodynamics Laboratory Bimonthly Progress Report: October 11, 1966." "Aero-Astrodynamics Laboratory monthly progress report : April 7, 1966." "Aero-Astrodynamics Laboratory monthly progress report : August, 1966." "Aero-Astrodynamics Laboratory monthly progress report : February, 1966." "Aero-Astrodynamics Laboratory monthly progress report : January 12, 1966." "Aero-Astrodynamics Laboratory monthly progress report : July, 1966." "Aero-Astrodynamics Laboratory monthly progress report : June, 1966." "Aero-Astrodynamics Laboratory monthly progress report : March 8, 1966." "Aero-Astrodynamics Laboratory monthly progress report : May, 1966." "Aero-Astrodynamics Laboratory monthly progress report : September, 1966." "Aerospace Vehicle Simulation and Checkout." "Aerospace Welding Standards for the Minutes of the Meeting of American Ordnance Association." "After the Moon - What? Minutes of the Manned Flight Awareness Seminar." "Air Force Surveys in Geophysics: The ARDC Model Atmosphere, 1956." "Alignment Tool Aids in Large Tank Fabrication." "All Digital Simulation of Saturn I, IB, and V: Boost Vehicle and Guidance Control Systems." "All systems 'go' for liftoff of Apollo 10." "Alloy designation" Table. "Altitude Simulation in Saturn SIV Space Testing." "America's Spaceport." "American Progress and Goals in Space," address by James E. Webb. "An Iterative Guidance Scheme and Its Application to Lunar Landing." "Analog Simulation of Saturn S-IB Stage Propulsion System Dynamic Characteristics." "Analysis and Projections of Space Vehicle Automatic Checkout and Launch." "Annual progress report :1966-1967." "Annual Report of Brown Engineering Company, Inc. For the Year Ended December 31, 1965." "Apollo - LEM Docking Drogue Assembly Static Structural Test." "Apollo 10 crew ready for return from space." "Apollo 10 in spotlight as CDDT is completed." "Apollo 10 to simulate lunar landing mission." "Apollo 11 Mission Profile." "Apollo 11 module comes back to downey home." "Apollo 4 Pre-Launch Press Conference." "Apollo 4 press kit." "Apollo 4 Spurs Lunar Landing Program." "Apollo 5 Post-Launch Press Conference." "Apollo 5 Pre-Launch Press Conference." "Apollo 6 Pre-Launch Press Conference." "Apollo 7 Mission Commentary." "Apollo 8 Mission (AS-503) : memorandum to A/Acting Administrator from MA/Apollo Program Director." "Apollo 9 carries lunar module." "Apollo 9 command module arrives home." "Apollo 9 flight ends; Astronauts return." "Apollo countdown begins on Monday." "Apollo Documentation Administration Instruction." "Apollo Logistic Support Systems." "Apollo Logistics Support System (ALSS) Payloads Summary Report." "Apollo Program Management Volume 3." "Apollo Program: Glossary of Acronyms and Abbreviations." "Apollo Saturn LIEF Operations Plan." "Apollo spacecraft Diagram." "Apollo Telescope Mount Fact Sheet." "Apollo Vehicle Propulsion Systems." "Apollo-LEM Docking Combined Probe and Drogue Assemblies Static Structural Test." "Apollo/Saturn consolidated instrumentation plan for AS-204/LM-1." "Apollo/Saturn Guide for the Preparation of Specifications: Volume I of II Volumes." "Appendix to Chapter II of a Survey of Various Vehicle Systems for the Manned Lunar Landing Mission." "Application of Data to Design: Design of Space Vehicle Structures for Vibration and Acoustic Environments." "Application of Nuclear Propulsion to the Mars Manned Landing Mission." "Application of Saturn Systems to Orbit Launch Operations." "Application of the Saturn V Launch Vehicle to Unmanned Scientific Exploration of the Solar System." "Approach in Achieving High Reliability for Saturn Class Vehicles." "Army Participation in the National Satellite and Space Program." "AS-203 Technical Information Summary." "Assessment of Risk for Engineering Change Decisions." "Assurance and Measurement of Space Vehicle Alignment." "Astronaut crewmen take part in final electronic checkout." "Astronaut trio sees 'successful' Apollo 9 mission." "Astronautics and Aeronautics April 1968: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics August 1969: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics December 1968: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics February 1969: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics July 1968: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics July 1969: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics November 1968: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics October 1968: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronautics and Aeronautics September 1969: A Chronology on Science, Technology, and Policy (HHR-23)." "Astronauts continue on greatest venture." "Astronauts set to preform key test of lunar landing technique." "Astronauts thank 7,000 during brief ceremony." "Automated PCM Data Processor Theory of Operation." "Automatic Pressure Transducer Calibration System." "Automatic Saturn V Page Test System." "Bendix: Yesterday, Today, and Tomorrow." "Bibliography of Research and Development Reports on the Centaur Program for Period 1958-1962." "Brooks Watson and Saturn's Steel Mountain." "Capabilities and Limitations of Space Communication Systems." "Carbon-Burning Nucleosynthesis at Constant Temperature." "Chemistry in Space Boosters" presentation given at Huntsville High School. "Chilldown Electrical System for S-IVB Space Vehicle." "Chronology of early Air Force man-in-space activity: 1955 - 1960." "Classification review of Saturn I/IB quarterly film report, no. 24." "Cleaning and Contamination Control." "Columbia and eagle prepared for launch." "Comments on Problems Relating to the Lunar-Landing Vehicle." "Common bulkhead drawing." "Communication from the President of the United States transmitting the report of the President's Materials Policy Commission, June 1952." "Communication-System Blackout During Reentry of Large Vehicles". "Company announces scholarship winners: Space Division places 9 of 21 boys and 16 girls." "Component Failure Effect on Systems: An Analytical Model". "Computer Controlled Power Application for the Saturn Launch Vehicle". "Computer Redundancy: Design, Performance, and Future". "Conditions contributing to stress corrosion [list] photograph." "Configuration Management-Definition". "Contract Status Report." "Contractor Program Procedure". "Contractor Program Procedures". "Contracts & Pricing: Saturn S-II Program". "Contracts for Saturn Upper Stages S-IV and S-V". "Corrosion Problems Associated with Space Launch Vehicles". "Corrosion problems associated with the Saturn space vehicles." "Countdown to Liftoff". "Countdown trials start for launch." "Craft destined for use in lunar landing mission." "Crew Briefing : Instrument Unit Stage Presentation". "D5-13197 manufacturing plan: AAP." "Data Sheet J-2 Rocket Engine." "Data Sheet: H-1 Rocket Engine." "Dec. 21 - 4:51 a.m. -One of great explorations of all time begins." "Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines." "Design and Development of a 1,500,000-Pound-Thrust Space Booster Engine." "Design and Development of a Zero-G Vapor Liquid Separator For Use in Cryogenic Fluid Power Systems." "Design and Use of Fault Simulation for Saturn Computer Design." "Design Concepts of Ground DDAS in Saturn 1B/V ESE." "Design of the Saturn S-IV Stage Propellant Utilization System." "Design, Development, and Fabrication of a Prototype Hydraulic Transformer." "Development and Utilization of Computer and Test Programs for Checkout of Space Vehicles." "Development Effort to Achieve Reliability." "Development of LOX-Hydrogen Engines for the Saturn Apollo Launch Vehicles." "Development of LOX/RP-1 Engines for Saturn/Apollo Launch Vehicles." "Development of Separable Connectors for the Saturn S-IV Stage." "Development of the NASA/Grumman Lunar Module." "Development of the Saturn S-IV and S-IVB Liquid Hydrogen Tank Internal Insulation." "Development Status for Arc Guidance, Weld Observation Systems, and a Review of Process Control Parameters." "Digest of FY-62 Funded Advanced Studies : July 1966." "Digest of FY-63 funded advanced studies : July 1966." "Digest of FY-64 Funded Advanced Studies: August 1966." "Digest of FY-65 Funded Advanced Studies:July 1966." "Digest of FY-66 Funded Advanced Studies: November 1966." "Digital Simulation of an Aerospace Vehicle." "Digital Transducers." "Dix ans D'exploration Spatiale." "Documentation List for Saturn Stages S-11." "Documentation Repository." "Douglas Aircraft Company Press release." "Dr. George Mueller: The Man Behind Manned." "Dr. von Braun/NASA HQ correspondence: July 1968." "Draft Script for Saturn I/IB Quarterly Film Report No. 25 (Covering July, August, September, 1965)." "Draft script Saturn I/IB quarterly film report no. 25." "Drawing number assignment" "Dual ceremonies honor astronauts of Apollo 9." "Dynamic Environments of the S-IV and S-IVB Saturn Vehicles." "Dynamic Loads of a Launch Vehicle Due to Inflight Winds." "Dynamic Problems in Launch Vehicles and Spacecraft." "Earth Orbital Workshop Capabilities Brochure." "Effects of High-Pressure Hydrogen on Steels." "Electrical support equipment" (ESE) [photograph]. "Engineering : Saturn S-II program" "Engineering Capabilities Presentation." "Engineering Safety Into Missile-Space Systems." "Engines for Manned Flight." "Evolution of a Space Capability." "Evolution of Aircraft." "Evolution of the Saturn Booster." "Evolutionary Steps in S-IVB Development." "Extensions of Saturn." "Fabricating the Saturn S-IC Booster." "Fabrication of Plenum Tanks by Explosive Forming and Electron Beam Welding." "Facilities Engineering for the National Aeronautics and Space Administration." "Facility Design for Handling Liquid Hydrogen for Space Vehicle Applications." "Fact Sheet : IBM Computer Will Direct Saturn Orbital Test Flight." "Failure Investigations of Large Liquid Propelled Rocket Engine Components." "Film script for Saturn I/IB quarterly film report no. 15." "Film script for Saturn I/IB quarterly film report no. 16." "Film Script for Saturn I/IB Quarterly Film Report, Nr. 22 (Covering October, November, December 1964)." "Film Script for Saturn I/IB Quarterly Film Report, Nr. 23 (Covering January, February, March 1965)." "Film script for Saturn quarterly film report no. 18." "Film Script for Saturn Quarterly Film Report, No. 19 (January, February, March) 1964." "Film Script for Saturn Quarterly Film Report, Nr. 20 (April, May, June) 1964." "Films List : NASA Motion Picture Film Service Area Five: Alabama - Kentucky - Louisiana - Mississippi - Tennessee." "Final readiness test underway on Apollo 11." "Final Script for Saturn I/IB Quarterly Film Report, No. 24 (covering April, May, June 1965)." "Final Script for Saturn IB Quarterly Film Report, No. 26 (covering October, November, December, 1965)." "Final Technical Report: Saturn V Derivative (S-IC/S-IVB/I.U.) Launch Vehicle System Study: Volume I." "First Annual Logistics Management Symposium: September 13 and 14, 1966." "First Hundred Seconds." "Five manned Apollo flights scheduled this year." "Flat Cable Engineering Studies for Saturn S-IVB Vehicles." "Flight Control Computer for Saturn Space Vehicles." "Flight Evaluation of the Command and Communication System Aboard AS-501." "Flight Software Development Laboratory." "Flight to test lunar module for moon landing." "Footprints on the Frontier." "Forecasting future military missions and their technological demands." "From Michoud to the Moon." "From Now On -." "Fulfilling the Aerospace Engineer's Responsibility for Product Reliability." "Functional Management in NASA." "Fundraising efforts underway at MTO." "Furnace Brazing of Liquid Rocket Thrust Chambers." "Furnace Brazing the F-1 Thrust Chamber for Apollo." "Future Projects Office." "General Electric/MTSD's First Five Years as Prime NASA Support Contractor at Mississippi Test Facility, Bay St. Louis, Miss." "George C. Marshall Space Flight Center Mississippi Test Facility Telephone directory 1965." "George C. Marshall Space Flight Center Mississippi Test Facility Telephone directory 1968." "George C. Marshall Space Flight Center Telephone Directory October, 1969." "Goddard patents: notes from von Braun to Slattery." "Government Grants & Contracts." "Ground Equipment to Support the Saturn Vehicle." "Ground testing at MSFC : research achievements review series no 9" "Guidance and Control of Saturn Launch Vehicles." "H-1 rocket engine: models H-1C and H-1D : technical manual engine data." "Helium Utilization in the Apollo/Saturn V Vehicle." "High Energy Missions for Saturn." "Highlights of General Electric's Participation in the U.S. Missile and Space Program." "Historical Notes on Oral History in NASA." "Historical Profile: North American Aviation, Inc." "Historical Sketch of MSFC." "Historical Summary on the Von Braun Missile Team." "Historical Summary: S & ID Apollo Program." "History of MSFC Reliability Philosophy." "History of Rocket Development Division." "History-making trio aboard USS Hornet." "Human factor systems." "Human Factor: ATM /Skylab." "Human Factor: ATM/Skylab." "Hundreds of Apollo employees submit Apollo names." "Huntsville: Space City, U.S.A." "IBM Mobile Room Lends Flexibility to Apollo Saturn Unit Fabrication." "Improving the Uprated Saturn I." "Information About Pratt & Whitney Aircraft Florida Research and Development Center." "Initial phase of new space station study are underway." "Inspection of Welds on S-II-1." "Instrument Unit in Crucial Test." "Instrument Unit Program Review : Saturn Instrument Unit." "Instrument Unit to Navigate Saturn IB's First Flight.". "Instrumentation Programming for Computer Controlled Digital Data Processing." "Interface Control Document Definition of Saturn SA-507 Flight Sequence Program." "Interface Problems in Space Experimentation." "Interview With Dr. Arthur Rudolph." "Interview with Dr. Wernher von Braun." "IU Presentation and Dedication." "IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses." "John F. Kennedy Space Center: A Selective Bibliography." "July 16th confirmed as definite for Apollo 11." "July 16th still set as Apollo 11's 'L-Day.'" "Juno V Space Vehicle Development Program (Phase I): Booster Feasibility Demonstration." "Juno V Space Vehicle Development Program." "Juno V Transportation Feasibility Study (U)." "Key Events in the Manned Lunar Landing Program." "Key MSFC Personnel for Potential Interview Efforts." "KSC Apollo/Saturn V Master Test Plan." "L-UT/Armb tower in pad position." "Launch Complex 34 Facilities Fact Sheet 05." "Launch Complex 37 Facilities Fact Sheet." "Launch Complex 39 Facilities Fact Sheet 03." "Launch Control and Checkout Equipment (LCCE) [photograph]." "Launch Information: Saturn S-IV and the RL10 Engine." "Launch Vehicle Engines Project Development Plan." "Launch Vehicle Recovery System Requirements." "Letter from Mr. David L. Christensen." "Letter to Dr. George E. Mueller." "Letter to Dr. Jerome B. Wiesner." "Letter to Dr. Keith T. Glennan." "Letter to Dr. Wernher von Braun." "Letter to Lieutenant General Samuel C. Phillips." "Letter to Mr. D. R. Spotz." "Letter to Mr. David Christensen." "Letter to Mr. David L. Christensen, Research Associate." "Letter to Mr. David L. Christensen." "Letter to Mr. Eugene M. Emme." "Letter to Mr. Frank L. Murphy." "Letter to Mr. George M. Low. and Joseph F. Shea." "Letter to Mr. Harrison A. Storms." "Letter to Mr. Helmut J. Horn." "Letter to Mr. Kurt R. Stehling." "Letter to Mr. Walter D. Sohier." "Letter to Professor John Logsdon." "Letter to Professor John M. Logsdon." "Letter to The President and White House." "Letter to the Vice President of the United States and White House." "Liquid Hydrogen Technology, J-2 Engine." "Liquid Hydrogen." "Liquid Rocket Engines." "Liquid Rocket Propellant Compatibility Testing." "Liquid Rockets." "List of Academic Theses Since 1961 Related to the History of Aeronautics and Astronautics." "List of Equipment, Components, Materials, and/or Services Now Being Developed, Fabricated or Performed." "List of Saturn-Apollo Suppliers of Critical Hardware." "List of Technical Documents, Papers and Articles Published in 1967." "List of Technical Papers and Articles 1958 Through 1962." "Listing of Historical Documents and Interview Tapes." "Little known engineer is father of 'Moon-Bug' idea." "LM System Description." "Lunar Applications of a Spent S-IVB/IU stage (LASS)." "M-45 casting alloy : Gyro stabilizer support." "Maintenance Data - How and What." "Man, Machine, and Automatic Test Operations." "Management matrix integrating logistics support planning events." "Management of the Space Program at a Field Center." "Management Plan for Saturn Vehicle System." "Management problems faced in making future manned space exploration decisions." "Management system" "Manned Launch Vehicle Development." "Manned Lunar Landing via Rendezvous." "Manned planetary flyby missions (based on Saturn/Apollo Systems) : executive summary report." "Manned space and lunar exploration." "Manned space flight program review : MSFC institutional report." "Manned Space Flight Program status for presentation to the Management Council." "Manned space flight schedules. Vol. III, launch vehicles : book 1, Saturn I." "Manned space flight schedules. Vol. III, launch vehicles : book 2, Saturn IB." "Manned space flight schedules. Vol. III, launch vehicles : book 3, Saturn V." "Manned space flight schedules. Vol. III, launch vehicles : book 4, engines." "Manned space flight schedules. Vol. VII, construction of facilities, MSFC : book 6." "Manned space flight schedules. Vol. VII, construction of facilities, MSFC : book 2." "Manned space flight schedules. Vol. VII, construction of facilities, MSFC : book 3." "Manned space flight schedules. Vol. VII, construction of facilities, MSFC : book 4." "Manned space flight schedules. Vol. VII, construction of facilities, MSFC : book 6, various locations." "Manufacturing Development Information Report." "Manufacturing history - LM-5." "Manufacturing Organizational Chart : Saturn S-II program." "Manufacturing plan : Saturn V : booster stage S-IC. Volume 1." "Manufacturing plan : Saturn V : booster stage S-IC. Volume 2." "Manufacturing plan for Saturn S-II, Stages 16-25." "Manufacturing problems with printed circuit boards and how to avoid them." "Manufacturing welding control by E. R. Seay, Group Engineer, Lockheed-Georgia Company." "Marshall analysis : DMS Market Intelligence Report." "Marshall in the Space Effort." "Marshall Space Flight Center personnel for potential interviews." "Master list of projects." "Master plan for documentation management and use." "Material : Saturn S-II program." "Materials in space exploration." "McDonnell Douglas S-IVB rocket for NASA's Saturn launch vehicle." "Measurements on the Saturn space vehicle." "Measuring instrumentation support." "Meeting with Huntsville community leaders, Morris Auditorium." "Meeting with the Director, Development Operations Division, ABMA, Huntsville : Memorandum for the Associate Administrator." "Memorandum : AAP experiment assignments - Case 600-1." "Memorandum : request for additives and comments on draft historical note 57." "Memorandum : S-II Stage Program Report from MA/Apollo Program Director to MA/Associate Administrator for Manned Space Flight." "Memorandum : Saturn I/IB quarterly film report no. 21." "Memorandum : Saturn I/IB quarterly film report no. 22." "Memorandum : Saturn I/IB quarterly film report no. 23." "Memorandum : Saturn I/IB quarterly film script review." "Memorandum : technical information summary concerning Saturn I vehicle SA-6." "Memorandum for Director of Space Flight Programs" related to the "Manned Lunar Landing Program." "Memorandum for Dr. Emme/EH from James E. Webb, Administrator." "Memorandum for Dr. Thomas O. Paine, Acting Director from George E. Mueller, Associate Administrator for Manned Space Flight, dated November 11, 1968." "Memorandum for General Ostrander." "Memorandum for Mr. Webb from George E. Mueller." "Memorandum for record : meeting to review problems with H-1 engines on S-IB-7 and S-IB-8." "Memorandum for the administrator." "Memorandum for the Associate Administrator: Artificial Gravity Considerations for Project Apollo." "Memorandum for the president: Responsibility and organization for certain space activities." "Memorandum for the record, from E. M. Cortright, Assistant Administrator for Programs." "Memorandum for the Vice President from (John F. Kennedy)." "Memorandum to Associate Administrator for Manned Space Flight for Acting Director." "Memorandum to Dr. Emme - EH through Mr. Shafter - G from Julian Scheer, Assistant Administrator for Public Affairs, National Aeronautics and Space Administration." "Memorandum to Dr. Eugene M. Emme, Code EH, NASA Headquarters, Washington, D. C. from Bart J. Slattery, Jr., Chief of Public Affairs." "Memorandum to Dr. Seamans from Mr. Holmes. Subject: F-1 engine combustion instability problems." "Memorandum to Margaret from Mrs. Bonnie Holmes, Secretary." "Memorandum to Mr. Hal Seawright, TS-PP, from Norman L. Cropp, Jr., Film Coordinator. Declassification of S-I/IB quarterly film report #18." "Memorandum to Mr. Horner from T. Keith Glennan, Administrator." "Memorandum, routing slip, and letter by Harold G. Russell, Colonel, USAF, concerning the Business Week article 'North American tries to advance under fire.'" "Memorandum: collection, preparation and submission of POP 65-3." "Memorandum: Indices to MSFC circulars and MSFC Administration regulations and procedures from Chief Management Services Office." "Memorandum: John F. Kennedy Memorial Library in Massachusetts." "Meteoroid measurements with Project Pegasus." "Methods for cleaning electronic components and subassemblies." "Meticulous engineering." "Michoud and Mississippi test operations : May 1965." "Michoud assembly facility and Mississippi test facility : volume II. 4th edition." "Michoud Assembly facility telephone directory : Boeing Launch Systems Branch, Chrysler Space Division, LTV Range System Div., Mason-Rust Engineering Company." "Michoud operations : historical operations: July 1, 1963 - December 31, 1963." "Milestones in cryogenic liquid propellant rocket engines." "Minimax control of large launch boosters." "Mission and facilities of Instrument Development Branch." "Mississippi test - torrents of flame." "Moon brought near by Apollo 8 mission." "Moon-bound" "MSC/Apollo program management" "MSFC contracts report : compiled from NASA Research and Technology Program Digest." "MSFC Manned Space Flight Program status for December 18, 1962 Management Council meeting." "MSFC Manned Space Flight Program status for presentation to the Management Council, March 26, 1963." "MSFC Manned Space Flight Program status for presentation to the Management Council." "MSFC project descriptions : 1967." "MSFC projects index by laboratory." "MSFC specifications, standards and procedures microfiche reference file index." "MSFC systems engineering capabilities (abstracts of reports)." "MSFC technical facilities history and description." "NASA establishes facility for Earth resources study." "NASA management programs." "New Liftoff date only change in Apollo 10 mission." "News from Rocketdyne : Project Saturn." "News release : Liquid Hydrogen." "Next stop : the moon." "NEXUS concept of a large reusable earth launch vehicle." "Noise reduction study in a scaled model acoustic test facility." "Nondestructive testing of space vehicle liquid propellant rocket engines." "North American Rockwell News: Space Division Skywriter: Volume 29 Number 37." "Nortronics Huntsville organizational chart." "Note to Dr. Mueller from Samuel C. Phillips." "NR executives hail technology exchange." "Nuclear engine design considerations." "Office memorandum : United States Government : RL-10 engine management arrangements." "Operational Experiences on the Saturn V S-IVB stage." "Opportunities for European Payloads on the Saturn Vehicle." "Orbiting research laboratory/logistics spacecraft checkout requirements study." "Organization chart of the Department of Defense - Directory." "Organization of a countdown" "Organization, programs, and activities, of the technical sections Nortronics - Huntsville." "Organizational charts for Rocketdyne, a Division of North American Aviation, Inc." "Organizational Structure and Mission of Aerospace Environment Division" "Outline of the capability of technical facilities and equipment at the George C. Marshall Space Flight Center." "Pan Am Clipper : Guided Missiles Range Division : December, 1964." "Part analysis program." "Payload integration for space experimentation." "Pershing (u): a report bibliography." "Personnel administration." "Pesco progress." "Philosophy and practices of reliability as applied in the design of the Saturn Instrumentation System." "Planning for strategic deterrence in the 1970s." "Plastics in space flight programs." "Pogo analysis of the Saturn Propulsion System." "Post-Apollo space program report: directions for the future." "Practicalities in automated manufacturing checkout." "Pratt & Whitney Aircraft RL10 liquid hydrogen rocket engine." "Pratt & Whitney Aircraft RL10 liquid hydrogen rocket engine" "Preliminary skeletal operations plan for Apollo :" a systems engineering support document. "Preliminary study of an unmanned lunar soft landing vehicle (Scientific Application)." "Press release : NASA starts development on ATM." "Press release 931A : Saturn S-IV first firing." "Problems associated with large scale high pressure testing." "Problems experienced in program management." "Problems in cryogenic pump design for space application." "Proceedings : second NASA-wide reliability & quality assurance meeting : NASA Headquarters, November 29 - December 1, 1966." "Procurement programs of Marshall Space Flight Center as related to DOD procurement and Space Administration support by DOD activities." "Program scheduling manual." "Program Submission FY-1969: Electronics Systems." "Project Apollo 7: news release." "Project Dynasoar (u): a report bibliography." "Project High Water." "Project Manager's Report." "Project Thor (u): a report Bibliography." "Propulsion : the key to moon travel." "Propulsion : the key to space travel." "Propulsion and Vehicle Engineering Laboratory monthly progress report : August, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : August, 1968." "Propulsion and Vehicle Engineering Laboratory Monthly progress report : December, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : Febuary, 1968." "Propulsion and Vehicle Engineering Laboratory monthly progress report : January, 1968." "Propulsion and Vehicle Engineering Laboratory monthly progress report : July, 1967. "Propulsion and Vehicle Engineering Laboratory Monthly progress report : July, 1968." "Propulsion and Vehicle Engineering Laboratory monthly progress report : June, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : March, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : March, 1968. "Propulsion and Vehicle Engineering Laboratory monthly progress report : May, 1966." "Propulsion and Vehicle Engineering Laboratory monthly progress report : May, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : November, 1967." "Propulsion and Vehicle Engineering Laboratory monthly progress report : October, 1966." "Propulsion and Vehicle Engineering Laboratory monthly progress report : October, 1967. "Propulsion and Vehicle Engineering Laboratory monthly progress report (April 1, 1966 through April 30, 1966)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (April 1, 1967, through April 30, 1967)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (August 1, 1966 through August 31, 1966)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (July 1, 1966 through July 31,1966)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (March 1, 1966 through March 31,1966)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (November 1, 1966 through November 30, 1966)." "Propulsion and Vehicle Engineering Laboratory monthly progress report (September 1, 1967 through September 30, 1967)." "Propulsion and Vehicle Engineering Laboratory monthly progress report, December." "Propulsion and Vehicle Engineering Laboratory monthly progress report, November." "Propulsion and Vehicle Engineering Laboratory monthly progress report, September." "Propulsion and Vehicle Engineering Laboratory monthly progress report" April. "Propulsion and Vehicle Engineering Laboratory monthly progress report" May. "Propulsion development problems associated with large liquid rockets." "Propulsion lecture." "Pumping boiling liquid hydrogen without cavitation." "Purchasing and contracting at the George C. Marshall Space Flight Center." "Quality assurance provisions for government agencies." "R & D directory for 1962 (NASA-MSFC Contracts-1962)." "Recent NASA experience with hydrogen engines." "Recoverable S-IB." "Redundancy employing majority voting for a Saturn servoactuator." "Reliability and quality management." "Reliability assessment of liquid rocket engines." "Reliability engineering program provisions for Space System contractors. Revision 2." "Reliability prediction in design decision." "Report From Mississippi." "Report of Ad Hoc panel on Man-in-Space." "Report on the Saturn-Apollo program." "Report to Mr. Sohier from Dr. Emme." "Report to the administrator, NASA on the Saturn development plan." "Report to the Congress from the President of the United States" "Repository index of engineering reports and procedures." "Request for approval to man the Apollo Saturn V Vehicle." "Research grants and contracts awarded to 25 : NASA news." "Response to any news media queries concerning MSFC S-II stage." "Resume - Werner K. Gengelbach." "Rocket engine selection criteria." "Rocket engine turbo pumps for space travel." "Rocket exhaust effects on radio frequency transmission." "Rocket motor" material list photograph. "S-IC heat shield illustration." "S-IC Saturn booster." "S-IC stage, S-II stage, S-IVB stage, instrument unit drawing." "S-II Engine." "S-IVB Saturn high energy upper stage and its development." "SAA program specification - case 218." "Safety engineering for the man." "Sat V growth and flexibility." "Satellite recovery system." "Saturn -- the lunar vehicle." "Saturn : DMS market intelligence report." "Saturn 1750 LB. Thrust ullage rocket engine." "Saturn and its mission." "Saturn and the exploration of space." "Saturn and the future." "Saturn and the Gulf Coast." "Saturn and the NASA space program." "Saturn Apollo applications program specification." "Saturn Apollo guidance error estimation." "Saturn ascending phase guidance and control techniques." "Saturn base heating review." "Saturn C-1 vehicle project development plan." "Saturn C-5, S-IC, stage fuel tank assembly." "Saturn data summary handbook." "Saturn display set: instruction manual." "Saturn history documentation: subject index." "Saturn I : the first generation of heavy launch vehicles designed for peaceful exploration of space." "Saturn I engine gimbal and thrust vector control systems." "Saturn I flight test evaluation." "Saturn I summary." "Saturn I workshop experiments." "Saturn I workshop, 1968." "Saturn I workshop, 1969." "Saturn I: The First Generation of Heavy Launch Vehicles Designed for Peaceful Exploration of Space." "Saturn I/IB Launch Vehicle Operational Status and Experience." "Saturn I/IB quarterly film report no. 24, April, May and June, 1965." "Saturn I/IB quarterly film report no. 24." "Saturn I/IB quarterly film report no. 25." "Saturn I/IB quarterly film report no. 26." "Saturn IB - Saturn V instrument unit technical facts." "Saturn IB : presentation to Little Rock Group." "Saturn IB ESE interlock system." "Saturn IB inflight photographic instrumentation system." "Saturn IB news reference." "Saturn IB orientation training manuel." "Saturn IB SA-217 reference launch vehicle." "Saturn IB/V Instrument Unit system description and component data: technical manual." "Saturn IB/V instrument unit." "Saturn illustrated chronology : April 1957 - August 1963." "Saturn illustrated chronology : April 1957 - November 1962." "Saturn instrumentation systems." "Saturn launch vehicle presentation." "Saturn launch vehicles : security classification guide." "Saturn Radar Altimeter." "Saturn S- II quality & reliability assurance : quality and reliability assurance" Organizational Chart. "Saturn S-IC annual progress report, 1964." "Saturn S-IC annual progress report, 1965." "Saturn S-IC booster : schematic." "Saturn S-II : annual progress report : 1 July 1962 through 30 June 1963." "Saturn S-II annual progress report 1 July 1963 through 30 June 1964." "Saturn S-II facilities organization." "Saturn S-II general manual." "Saturn S-II ground support equipment inspection manual." "Saturn S-II stage program plan." "Saturn S-IV cryogenic weigh system. Part I : propellant utilization." "Saturn S-IV cryogenic weigh system. Part II : weigh operations." "Saturn S-IV cryogenic weigh system. Part IV : safety." "Saturn S-IV engines." "Saturn S-IV first firing." "Saturn S-IVB quarterly technical progress report." "Saturn SA-1 flight and its instrumentation." "Saturn ST-124-M inertial guidance platform." "Saturn stages S-II : July 7, 1961 : Minutes of the phase II pre-proposal conference for stage S-II procurement." "Saturn system study II." "Saturn technical information handbook. Volume III of four volumes : SA-203." "Saturn television system for SA-6." "Saturn V : non-stage procured launch vehicle ground support equipment." "Saturn V America's moon rocket." "Saturn V Apollo Flight Configuration." "Saturn V Apollo lunar orbit rendezvous mission." "Saturn V derivatives." "Saturn V first stage annual progress report : fiscal year 1966." "Saturn V First Stage Annual Progress Report: Fiscal Year 1968." "Saturn V ground winds program." "Saturn V inboard profile : Launch escape system flight separation." "Saturn V interface management." "Saturn V launch vehicle ground support equipment fact booklet." "Saturn V quarterly progress report : January - March." "Saturn V rocket booster test stand at MSFC." "Saturn V S-IC stage engine gimbal actuation system." "Saturn V semi-annual progress report July - December, 1967." "Saturn V semi-annual progress report July-December, 1966." "Saturn V service arms : preliminary engineering report." "Saturn V space program and aluminum welding technology." "Saturn V specification cross reference index." "Saturn V specification index." "Saturn V stage progress." "Saturn V vehicle electronics." "Saturn Vehicle Cryogenic Programs." "Saturn vehicles for Apollo photograph." "Saturn: draft." "Saturn/Apollo contract change : letter from George E. Mueller to Morton E. Henig." "Science and technology - keys to economic progress." "Science and technology advisory committee for manned space flight." "Section III of Saturn C-1 vehicle project development plan." "Security classification review of quarterly film report no. 23." "Security classification review of Saturn I/IB quarterly film report, no. 25." "Selected methods for uprating Saturn vehicles." "Sensitivity of rocket engine stability to propellant feed system dynamics." "Signal distribution in automatic checkout systems." "SII, with all spray foam insulation MTF-bound." "Six-engine cluster of the Saturn S-IV rocket." "Some computer applications in Saturn stage checkout." "Some select physiological, anthropometric, and human engineering data useful in vehicle design and logistic problems of space flight operations." "Space age management or maintenance of technical capability during a period of retrenchment." "Space and the working woman." "Space Division, North American Rockwell Corporation Organizational Chart." "Space flight : first draft." "Space flight projects - today and tomorrow." "Space sparks a renaissance in education." "Space Station operations analysis using Gemini-Titan II-Agena." "Space vehicle systems" research and technology. "Space vehicle test stands." "Spacecraft television ground data handling system." "Sperry Rand Earth Orbital Workshop Capabilities" Brochure. "Sperry Rand monthly progress report for July, 1969." "Stability analysis of Apollo - Saturn V propulsion and Structure feedback loop." "Stabilized mechanical properties [table] photograph. "Standard procedure for using units of mass, weight, force, pressure and acceleration." "Standards of conduct for NASA employees." "Statement of George E. Mueller, Associate Administrator for Manned Space Flight before the Committee on Aeronautical and Space Sciences, United States Senate." "Statement of George E. Mueller, Associate Administrator for Manned Space Flight." "Static test of Saturn V S-IC : news release. "Statistical model for Saturn electrical support equipment mission availability." "Structural problems of large space boosters." "Structure of the NASA/Grumman lunar module." "Survey of Saturn stage test and checkout computer program development." "System description for Saturn vehicle (SA-1 through SA-4)." "System engineering propulsion, III-C-1." "System safety handbook." "Systems applications in orbital launch operations." "Table I : chemical composition of experimental alloys." "Table II : comparison of typical mechanical properties of experimental alloys with commercial alloys." "Table IV : chemical composition of M-45 and other high strength aluminum casting alloys." "Table V : mechanical properties of aluminum casting alloys." "Technical facilities & equipment digest." "Technical History of Saturn." "Technical Information Summary Apollo 8 (AS-503) Apollo Saturn V Space Vehicle." "Technical information summary Apollo-10 (AS-505) Apollo Saturn V space vehicle." "Technical Information Summary Apollo-9 (AS-504) Apollo Saturn V Space Vehicle." "Technical information summary concerning Saturn vehicle SA-3." "Technical problems in on-board checkout systems." "Technical survey of ABMA activities." "Technician inspects an RL10 liquid hydrogen engine." "Technique for reliability circuit design review in space electronics." "Techniques of implementing launch automation programs" (Saturn IB space vehicle system). "Technological problems of the Saturn class vehicle." "Telegraphic message : inspection requirements for S-II-1 and S-II-2 at KSC." "Telemetry system design for Saturn vehicles." "Telemetry system for Saturn S-I stage development." "Test Laboratory monthly progress report : March, 1967." "Test Laboratory monthly progress report : May, 1967." "Test Laboratory monthly progress report" April. "Test Laboratory monthly progress report" August. "Test Laboratory monthly progress report" December. "Test Laboratory monthly progress report" Febuary. "Test Laboratory monthly progress report" January. "Test Laboratory monthly progress report" July. "Test Laboratory monthly progress report" June. "Test Laboratory monthly progress report" October. "Test Laboratory monthly progress report" September. "Test Laboratory progress report" Febuary and March. "Test Laboratory progress report" March and April. "Test Laboratory progress report" May and June. "Test operations:" Organization Chart. "Test procedure validation by computer simulation." "The Astrodynamicist's Role vis-a-vis the Systems Engineer." "The Case for Compatibility." "The Challenge of Change vs the Control of the Process." "The Common Bulkhead for the Saturn S-II Vehicle: Unique Manufacturing Effort Adds to Space-Age Hardware Technology". "The development of a bonded common bulkhead for Saturn." "The development of a checkout language : ATOLL." "The Development of Servovalves with Improved Reliability for Space Vehicles." "The development of the Saturn system safety program." "The ease (E's) of implementation of the Safety Program at the Marshall Space Flight Center." "The history of Army missile development." "The IBM Clean Room Comes of Age." "The impact of manufacturing on design as related to accessibility." "The Influence of Apollo/Saturn V Launch Operations on Lunar Site Selection: Case 330." "The instrumentation of space vehicle in connection with the successful Saturn flight tests." "The Iterative Guidance Law for Saturn." "The J-2 Liquid Hydrogen Rocket Engine." "The Missile gap : a study of the formulation of military and public policy." "The NASA/Grumman Apollo lunar module" "The potential bio-medical applications of Saturn nondestructive test methods." "The production of large tanks for cryogenic fuels" "The program manager's problem" "The reliability of the all-up concept." "The reliability picture at Marshall Space Flight Center - philosophy, staffing and management. Proposed talk to Orlando Section American Society for Quality Control." "The role of simulation in the development of an automatic checkout system" "The role of the NASA-MSFC Manufacturing Engineering Laboratory in the development of space projects." "The role of the S-IVB in the Apollo and past Apollo programs." "The role of weighing in the development and firing of missile and spaceships." "The Saturn IB launch vehicle system." "The Saturn launch vehicle family." "The Saturn launch vehicles." "The Saturn S-II." "The Saturn V mission and Alabama." "The significance of parameters affecting the heat transfer to the liquid hydrogen in the Saturn S-IVB stage for the lunar orbit rendezvous mission." "The toughest weld of all" S-II stage manufacturing. "The TV system for the Apollo telescope mount." "The U.S. manned space flight program: Mercury, Gemini, Apollo." "The uprated Saturn I - its growth potential & future role in space." "The use of wind shears in the design of aerospace vehicles." "Thermal models of Jupiter and Saturn" "This is Your Chrysler Saturn Story." "Timing and countdown systems handbook." "Toftoy statement to Senate Investigation Committee": Development of the Nike system. "Tool and Engineering Branch publication report." "Tooling for aerospace application." "Transportation of Douglas Saturn S-IVB stages." "Trends in procurement" by Garland Buckner. "U.S. Aerospace Program: missions and projects as of January 1, 1966." "Ultra high strength composite materials." "United Aircraft Quarterly Bee-hive:" January 1962, Volume XXXVII, Number 1. "United Aircraft Quarterly Bee-hive:" Spring, 1962: Volume XXXVII, Number 2. "University and research institute contracts awarded by MSFC." "Use of tank mounted booster pumps for providing NPSH to turbopumps operating in a radiation environment." "Uses of Saturn." "Vibration and acoustic environment characteristics of the Saturn V launch vehicle." "Vol. IV 3rd edition Management Information." "Von Braun's move ended Moon-Bug NASA dispute: rocket pioneer had favored earth-orbital rendezvous plan." "We're winning the race with Russia." "Welcome back planned for 'Gum Drop' crew." "Welding cryogenic materials for aerospace applications." "Welding for aerospace application : a panel discussion." "Where are we going in space management." "Why internal insulation for the Saturn S-IV liquid hydrogen tank?." "X-ray television inspection of aerospace weldments : Television x-ray image enlargement system for inspection." Convective Energy Transport in Stellar Atmospheres: A Convective Cell Model. Guided Missiles Range Division Clipper , vol. 2, no. 3, October 1961.1962 Chronological History, NAA Space and Information Systems Division, Downey, California. 1966 Chronology of Marshall Space Flight Center. A "Think Clean" training program. Acceptance Checkout Equipment - Spacecraft (ACE-S/C) news release. Active contracts list, Propulsion and Vehicle Engineering Laboratory. Additional script information for Saturn I/IB Report no. 19. Advanced Astrionics project review. Apollo 10 press kit. Apollo 10/AS-505 mission chart. Apollo 5 press kit. Apollo 8 Mission Operation Report. Apollo Support Program: Phase 1: Apollo Terminology Standards Final Study Report. Apollo/Saturn Lunar Landing Program. Artist's Conception of the RL10-powered Saturn S-IV Stage. Bibliography of AEDC J-2 engine test reports. Bibliography of RIFT documentation, 1968. Boeing and Apollo 11. Boeing Magazine, vol. XXXIII, no. 11, November 1963. Boeing Magazine, vol. XXXIV, no. 10, October 1964. Boeing Magazine, vol. XXXIV, no. 11, November 1964. Boeing Magazine, vol. XXXIV, no. 12, December 1964. Boeing Magazine, vol. XXXIV, no. 4, April 1964. Boeing Magazine, vol. XXXIV, no. 9, September 1964. Boeing Magazine, vol. XXXV, no. 1, January 1965. Boeing Magazine, vol. XXXV, no. 10, October 1965. Boeing Magazine, vol. XXXV, no. 11, November 1965. Boeing Magazine, vol. XXXV, no. 12, December 1965. Boeing Magazine, vol. XXXV, no. 2, February 1965. Boeing Magazine, vol. XXXV, no. 5, May 1965. Boeing Magazine, vol. XXXV, no. 7, July 1965. Boeing Magazine, vol. XXXVI, no. 1, January 1966. Boeing Magazine, vol. XXXVI, no. 6, June 1966. Boeing Magazine, vol. XXXVI, no. 8, August 1966. Boeing Magazine, vol. XXXVII, no. 3, March 1967. Boeing Magazine, vol. XXXVII, no. 7, July 1967. Boeing Magazine, vol. XXXVIII, no. 1, January 1968. Boeing Subcontractors on Project Apollo. Booster instrumentation for static firing. Briefing for Apollo 10. Brown Engineering Company 1964 Annual Report. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 1. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 10. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 11. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 12. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 13. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 14. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 15. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 16. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 17. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 18. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 19. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 2. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 20. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 3. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 4. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 5. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 6. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 7. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 8. Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 9. Combustion Oscillations in F-1 Engine. Combustion oscillations in the F-1 engine, monthly report. Comments on SA-5 mission. Congressional inquiry regarding the S-II-T accident at the Mississippi Test Facility : letter to the honorable Clinton P. Anderson, Committee on Aeronautical and Space Science, United States Senate from James E. Webb, Administrator. Contact points within the NASA for exchange of information on lunar program matters. Contract let for $8 million for work relating to upper stages of Saturn rockets : news release. Contractor Program Procedures: Contract NAS8-5608; DRL 067, Line Item 7; DRL 007, Line Item 7. Contractors over $700,000 that made contribution to Saturn. Development of LOX/RP-1 engines for Saturn/Apollo launch vehicles. Differences of configuration in successive Saturn IB and Saturn V vehicles- case 330. Directory Chart : NASA/MSFC Manager's Office. Double seal insulation [drawing] photograph. Douglas Aircraft news release. Dr. von Braun's calendars and scrapbooks indicate that these were his personal contacts with President Kennedy, Vice-President Johnson and members of their immediate staff. Dr. von Braun's oral history interview transcript - Kennedy Library: memorandum. Draft of "Building the Moon Rocket." DX priority: memorandum. F-1 engine photograph. Film script for Saturn C-1/C-1B quarterly film report no. 13 (covering July, August, September, 1962). Film script for Saturn quarterly film report no. 10 (covering October, November, December, 1961). Film script for Saturn quarterly film report no. 11 (covering January, February, March, 1962). Film script for Saturn quarterly film report no. 12 (covering April, May, June, 1962). Film script for Saturn quarterly film report no. 9 covering July, August, September, 1961. Final Apollo 11 Lunar Surface Operations Plan. General O'Connor's address to the Huntsville Rotary Club. Huntsville Isascope: Volume V, No. 9. IBM Apollo/Saturn Press information. Interview with Bauer. Interview with Dieter Grau. Interview with Ed Mims. Interview with G.A. Phelps (Seal Beach?). Interview with H. Paul. Interview with Newell. Interview with Schwartz (chief engineer?). Interviews with Fontaine and Attinello, Davenport, Rocketdyne. Interviews with Sawyer and Kudebeh (Rocketdyne?). Interviews with Shields and Davenport (Rocketdyne?). Interviews with Weidner and Neubert. Interviews with Wernher von Braun conducted by Dr. Emme and T. Ray. Letter to Dr. Hugh Odishaw. Letter to Dr. Wernher von Braun. Letter to Honorable James E. Webb, Administrator, National Aeronautics and Space Administration from W. K. Wilson, Jr. Letter to Mr. David L. Christensen. Letter to Mr. Frank L. Murphy. Letter to Mr. J. L. Atwood. Letter to the Honorable James E. Webb, Administrator, National Aeronautics and Space Administration from Kurt R. Stehling. Management plan and competition for second stage for Saturn. Memo from William A. Fleming to Robert Seamans concerning an "Aerojet proposal for 1,000,000 pound thrust hydrogen oxygen engine." Memorandum for Dr. Mueller from Robert C. Seamans. Memorandum to Dr. Seamans, Dr. von Braun, Mr. Donlon, and Mr. Gilruth. Memorandum to update the "Apollo/Saturn Logistics Support Requirements Plan." Meteorites and ballistics. Michoud Assembly Facility Historical Report, January 1, 1967-December 31, 1967. Organization charts of ABMA during 1957-1960. Postflight Analysis of Saturn Telemetry Systems. Preservation, shipment & recovery of the Saturn booster. Press Kit: Project Apollo 6 (To be launched on or after Apr. 3). Press Release : S-IC simulator--Immediate release. Program Planning and Control : Saturn S-II program Organizational Chart." Propulsion and Vehicle Engineering Laboratory Monthly Progress Report for Period April 1, 1968 Through April 30, 1968. Publication listing. Reproduction of "Apollo Interface Control Document Log." S-IVB cutaway and J-2 engine." Saturn and lunar flight. Saturn AS-501 evaluation bulletin No. 1, November 14, 1967. Saturn I workshop. Saturn IB launch project development plan. Saturn Launch Vehicles Astrionics System Handbook, 2nd revised edition. Saturn Launch Vehicles Astrionics System Handbook. Saturn V history team at the Apollo 10 launch. Saturn V management information : August 1964 : Volume VI. Saturn V news reference. Saturn V project development plan : November 1967. Script for Saturn C-1/C-1B quarterly film report no. 14 (covering Oct., Nov., Dec., 1962). Source credibility and personal influence in three contexts : a study of dyadic communication in a complex aerospace organization. Space age vision [photograph]. Space Stations/Platforms/Workshop (U): A Report Bibliography. Space vehicles for the peaceful exploration of the inner solar system; Memorandum to Mr. K. K. Dannenberg from Joe M. Jones. Spaceflight: DDC report bibliography. Spaco, Inc. Annual Report, 1965. Survey of Automatic Checkout Systems for Saturn V Stages. System Safety Plan, Industrial Operations, Marshall Space Flight Center. Technical facilities and capabilities 1969. Technical information Summary Apollo-11 (AS-506) Apollo Saturn V Space Vehicle. Technical information summary of the Apollo Saturn 1B flight vehicle. Technical Reports" Bibliography. Telegraphic message containing an Apollo Program Flash Report. Test laboratory Monthly Progress Report: November 1, 1967 through November 30, 1967. The "Apollo/Saturn Data Handbook." The "Apollo/Saturn Guide for the Preparations of Specifications: Volume II of II Volumes." The History of Thor. The Post-Apollo Space Program: Directions for the Future. Theoretical liquid propellant performance calculations Transatel. Unofficial Directory: Government, Industry, and University Contacts in Management Research and Engineering. Various organization charts of NASA-MSFC during 1960-1969. Visual aids library slide guide. Volume II Appendices for the Saturn V Derivative Launch Vehicle System Study. Von Braun, Wernher, Interview Outline.
Description
Select... For release Thursday P.M., January 11, 1968. "Building the Moon Rocket" was presented at the National Machine Tool Builders Association Meeting, Doral Beach Hotel, Miami, Florida on November 3, 1965 by Dr. Mathias P.L. Siebel, the Deputy Director, Manufacturing Engineering Laboratory. There are handwritten notes throughout. "Carbon-Burning Nucleosyntesis at Constant Temperature" is part of the Orange Aid preprint Series in Nuclear Astrophysics, August 1968. The abstract states "Syntesis of elements during thermonuclear burning of carbon is examined at a series of temperatures (T=0.6, 0.8, 1.0, 1.2, 1.4) and for several initial compositions. Recent eperimental results (Ptterson, Winkler, and Zaidins 1968) for the 12C+!@C reaction are used. A general method for numerical solution of nuclear-reaction networkds is described. At the higher temperatures in the range now thought to be appropriate for carbon burning in stars, "Monthly progress report : April 7, 1966." "Monthly progress report : March 8, 1966." "Speech presented by Col. John R. McCombs regarding administrative conduct and how they should handle contracts. "The Case for Compatibility" is a paper by Robert L. Smith, Jr., who worked in Quality and Reliability Assurance Laboratory at George C. Marshall Space Flight Center. The summary states, "Ever since the use of missiles and space launch vehicles began, questions have existed in every program regarding the similarity between upstream (e.g., manufacturing, static firing ) and launch site checkout equipment. Programs have existed which utilized nearly identical equipment for both uses; other programs have existed in which any resemblance of the equipment was probably coincidental. Many factors have entered the final decisions, not the least of which were economic and schedule considerations, and, in some instances, the organizational structure of the developer." "This report outlines, through a series of sketches with accompanying text, the general features of the SA-203 Launch Vehicle and information on launch preparation, the launch facility and mission peculiar experiments." "This technical note concerns some of the problems encountered with the landing of a payload on the moon. The main problem areas such as guidance, velocity control and impact considerations are discussed. Although no final conclusions or designs are intended, it is hoped that the material presented will serve as a guide for future detailed work." 6Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California. 8 x 10 inch Black & White photograph. MS-G 103-63 Nov. 22, 63 is on the photograph. Displays the evolution of space-rocket designs side-by-side. 8 x 10 inch black and white diagram of the Saturn booster engines. 8 x 10 inch black and white diagram of a Saturn fuel-tank assembly cross-section. 8 x 10 inch black and white diagram of an Apollo spacecraft, each section labled for easy identification. 8 x 10 inch black and white diagram of the JII engine and the Saturn IV. 8 x 10 inch black and white diagram of the Saturn II engines. 8 x 10 inch black and white photograph including a table that displays the stabilized mechanical properties of the following alloys: :LA-141 and LAX-933. 8 x 10 inch black and white photograph of a graph displaying different alloys and comparing their 'nominal composition weight per cent' to one another. 8 x 10 inch black and white photograph of a gyro stabilizing support. 8 x 10 inch black and white photograph of a rocket motor material list. The weight of the material is measured in pounds. 8 x 10 inch black and white photograph of a table comparing the tensile strength of each alloy in relation to a desired goal. 8 x 10 inch black and white photograph of a table detailing the tensile strength, tensile yeild, elongation per cent and charpy impact of alloys. 8 x 10 inch black and white photograph of a table reperesenting the chemical composition of alloys M825 and M826. 8 x 10 inch black and white photograph that displays a table of two elements and their molecular makeup. Table includes the alloy of LA-141 and LAZ-933. 8 x 10 inch black and white photograph which displays an image that includes the plate, bar and the magnification of the bar to display its molecules. 8 x 10 inch black and white photograph; This is a cutaway drawing of the bulkhead with information about the LH2 tank skin, insulation, Aft LOX bulkhead, 2014-T6 alum skin and fiberglass core. Part of an envelope with photos accompanying C. E. Cataldo paper "Materials in Space Exploration." 8 x 10 inch black and white photograph. 8 x 10 inch black and white photograph. Contains images of the Saturn V, Saturn IB and Saturn I in reference to one another 8 x 10 inch black and white photograph. A photograph of a list of things contributing to stress corrosion. Referenced by "Materials in Space Exploration." Is part of envelope containing photos accompanying C. E. Cataldo paper "Materials in Space Exploration." 8 x 10 inch black and white photograph. A photograph of a workspace. 8 x 10 inch black and white photograph. Engine parts are labeled. 8 x 10 inch black and white photograph.; Image includes dimensions and labels of exterior features of the rocket. 8 x 10 inch black and white photograph.; Drawing contains information about the modified epoxy adhesive, aluminum film, mylar film, perforated phenolic honeycomb core, tank skin, mylar honeycomb core, polyurethane adhesive, weight and thermal conductivity.; Photo negative no. 651746 M-268. 8 x 10 inch black and white photograph.; Images included are: A-3 oxygen-hydrogen, H-1 oxygen-kerosene, J-2 oxygen-hydrogen, F-1 oxygen-Kerosene, M-1 oxygen-hydrogen. The thrust pounds is also listed.Shows them in reference to a human as a scale. A basic description of the Saturn rockets alongside diagrams for context. A book containing various articles surrounding the activities and achievements of the Saturn program up to January, 1962. A book containing various articles surrounding the activities and achievements of the Saturn program up to Spring, 1962. A book written with the key focus being how technology and science and its progress can aid in the growth of the economy. A brief history and purpose of nondestructive methods followed by a discussion of those methods. A brief sketch of the development of the equations for a weighted least squares estimator is given, the equations for both collective and recursive estimators being included. Four possible problem sources that may be encountered in the application of the estimator are identified. Various "success" parameters are defined in an attempt to predict the success with which, the method has been applied. The application of the estimation technique to the problem of computing various error parameters associated with the ST-124M guidance platform is described with the numerical results obtained using a manufactured data case are presented. These results are used to form conclusions about the effectiveness of the "success" parameters and preferred approaches to the problem of system evaluation using techniques of estimation theory. A brochure designed to depict a competence and capability in the area of large earth-orbital workshops. A collection of articles, one of which musing about the landing on/colonization of Mars in the future. A collection of organization charts from years 1960 to 1969. A collection of progress reports covering a large number of projects within the month of August, 1966 A collection of progress reports covering a large number of projects within the month of July, 1966 A collection of progress reports covering a large number of projects within the month of March, 1966 A collection of progress reports covering a large number of projects within the month of November, 1966 A collection of various graphs, resumes and recordings for space vehical systems. A collection of various procedures. Archive copy is a photocopy. There is no continuous numbering in this document. A computer system was designed to allow test engineers to progressively employ automation in the checkout of the Uprated Saturn I and Saturn V space vehicle programs and still allow manual control of the checkout process. A two-computer system was selected by National Aeronautics and Space Administration, and the International Business Machines Corporation was chosen to provide the programming engineering necessary to implement these objectives. Space vehicle checkout, prior to launch, may be characterized by controlling, monitoring, and testing the vehicle and its subsystems through the use of ground support equipment (GSE).; IBM Huntsville Library.; Presented at AIAA Conference, XVIIth International Astronautical Congress, Madrid, Spain, October 10-15, 1966 by Edward A. Robin, Manager, Vehicle Test Programming Department. A datasheet describing the function of the J-2 rocket engine. A design report which displays and explains how the Spacecraft Television Ground Handling System functions, is designed and what it might be used for in the future. A directory of different projects with descriptions underneath. A document recounting the history of the Rocketdyne Development Division A document reporting various space vehicle corrosion issues. Original is photocopy. A guidance scheme for vehicle flight from lunar orbit to a prescribed point on a spherical, non-rotating moon is presented. The equations of motion have been simplified only to perm it a closed solution for the thrust magnitude and thrust direction. The trajectory computations them selves are made under more realistic and accurate assumptions and are not included. A handwritten note on the title page notes that the document was received from Earl F. Rodriguez, General Electric Co., MTSD in Bay St. Louis. Includes a chronology of General Electric activity in south Mississippi. A history and description of the Michoud Assembly Facility in New Orleans, Louisiana. A history of Pratt and Whitney Aircraft Florida Research and Development Center. A history of the IBM's Space Systems Center clean room and a description of its uses. A letter to Jame E. Webb proposing that the first LEM that lands on the moon to be named after President Kennedy." A list of critical hardware from Saturn-Apollo Suppliers. A list of film reports covering the months of April, May and June of the year 1965. A list of films oriented towards the National Space Program and other related topics. A list of images with detailed descriptions of what they are and their histories. A list of the various contractors over $700,000 involved in the Saturn V production process, in addition to contract numbers and addresses. Archive copy is a photocopy. There are some handwritten notes in ink on some of the pages. A man-in-the-loop computer facility has been created using a digital computer, display terminal,and space vehicle flight computer to enable programmers to check out flight programs in a simulated space flight environment. The simulation requires a real time multi-programmed environment, which is supplied by a control system capable of scheduling programs on 32 levels of priority interrupt as well as answering demands for service at the display terminal. A special interface device permits visibility and control of the flight program as it executes in the flight computer. On-line inputs from the programmer at the display terminal and outputs from data collection and reduction routines to the display screen are executed in real time. The Flight Software Development Laboratory has proved to be very useful in reducing program preparation time and increasing flight program confidence. A news article describing that Apollo 10's goal is to simulate a lunar landing in preparation for the real mission. A news article detailing a ceremony in which astronauts thank the crew who built their rocket. A news article detailing a program for Apollo staff to name command modules. A news article detailing a Technology Exchange event held by North American Rockwell Corperation. A news article detailing the 'welcome back' ceremony for the nine astronauts who had just returned from a 10-day mission. A news article detailing the festivities planned upon the return of nine astronauts returning from a 10-day mission. A news article detailing the final preparation and readiness tests for the Apollo 11 rocket and crew. A news article detailing the new facility NASA constructed, touching on the project its meant for. A news article detailing the new space station project. A news article detailing the progression of the Apollo 11 mission and its preparation for a moon-landing. A news article detailing the recovery of the Apollo 11 crew by the USS Hornet. A news article detailing the return of the Apollo 11 module to Downey and the plans to set it up as a display. A news article detailing the scheduled launch for the Apollo 11. "Eagle" is the name of the lunar module and "Columbia" is the name of the service module. A news article detailing the winners of scholarships from a competition held by Space Division. This contest was held for the children of Space Division employees. A notation in the upper lefthand corner states "For the record: These are Dr. von Braun's comments to present to President Kennedy during his visit at Cape Canaveral, Fla., Nov. 16, 1963." A handwritten note is in the upper right corner. It appears that some of the pages to this document are missing. a note to Dr. Mueller from Samuel C. Phillips regarding the designations of space vehicles. A number of considerations are necessary in instrumentation programming, many of which are either not applicable or applicable to a lesser degree in other types of programming. This paper discusses these problems in general terms and illustrates how they have been dealt with specifically. The latter is done by describing the programming and operation of a data reduction system. A Part of the development of the Saturn S-IV/S-IVB stage the Douglas Aircraft Company has pioneered in the development of the cryogenic common bulkhead. The term common bulkhead is derived from the design function of the bulkhead, which is to separate the two cryogenics, liquid hydrogen and liquid oxygen, in a single tank, thereby shortening the stage and eliminating the necessity for two separate bulkheads and the associated interstage structure. The common bulkhead is structurally adequate to withstand both the thermal and the pressure loads from both the hydrogen and the oxygen tanks, and it has sufficient insulation properties to prevent the liquid hydrogen from freezing the liquid oxygen. Another benefit from the common bulkhead is that it permits a reduction in the total length of the vehicle, thereby reducing the bending moments. a press release which focuses around the Apollo 9 flight and what role the ST-124-M inertial guidance platform has in it. A press-release detailing the successfuly firing and the specfic launching information of the Saturn I-V rocket-launch. A report to Congress from White House regarding the accomplishments of NASA. A rocket from the George C. Marshall Space Flight Center will carry the first American to the moon, and the deadline is 1970. Because of the Center's expanding role in space, there are increasing requests for information about our activities. This brief historical sketch should help to answer questions about our past, our present, and our hopes for the future. Marshall Space Flight Center (MSFC) is the largest installation of the National Aeronautics and Space Administration (NASA). The Marshall Center is NASA's agency responsible for large space rockets and related research. MSFC employs about 7500 civil service employees with an annual payroll of more than {dollar}82 million. In addition approximately 4300 contractor employees work for MSFC on the Arsenal, earning an estimated {dollar}43 million. The Center occupies about 1800 acres near Huntsville, Alabama; in this large area are 270 buildings with floor space totalling about 4,000,000 square feet for a real estate and property value of about {dollar}325 million. MSFC's 1966 fiscal year budget was {dollar}1.8 billion. Obviously MSFC has much human and monetary worth behind United States round trips to the moon and beyond. In addition to its size, MSFC is unique because it has a large rocket development team with more than three decades of experience. Prior to the rocket work that dates back to Peenemuende [sic] the world heard little and cared less concerning rockets and space. As a group Marshall has always thought big. It has worked together as a group, and equally well with fellow scientists throughout the Free World, to get the most into space soonest. This is why there is increasing interest in larger and larger rockets and rocket programs from our Center, a fact generating more and more questions about our Center, and in turn generating a "workload" request for this sketch by the Historical Office. We hope that you enjoy our historical sketch, which could as well be entitled "Closer and Closer Views of the Moon and Beyond." David S. Akens, MSFC Historian. A sensitive new television X-ray image enlargement system has been developed under sponsorship of Watertown Arsenal Laboratories (Army Materials Research Agency) by the Department of Welding Engineering of The Ohio State University. Now commercially-available through Philips Electronics Instruments (Norelco), complete systems have been in service since January 1963 in aerospace, electronic, and other facilities. Such users report highly- satisfactory performance and unusual reliability in service. The new X-ray system permits in-motion or stationary examination of critical aerospace materials, components, and systems such as sheet materials, weldments, brazed joints, electronic components, printed circuit assemblies, small mechanisms, and biological specimens. A series of french articles related to the space program. A summary found following the errata page reads: "This paper presents a second look at the subject of the man-machine relationship in automatic test operations. 'Man, Machine, and Automatic Test Operations' was presented by the writer at Battelle Memorial Institute in November of 1963...It is the purpose of this second look at the man-machine interface to pinpoint those concepts which have proven their worth with time and those concepts which have proven to be weak, and as a result modified with time." This paper was prepared by George F. Meister, Jr. A technician inspects an RLlO liquid hydrogen rocket engine OD the assembly floor. of Pratt & Whitney Aircraft's Florida Research and Development Center. The 115,000-pound-thrust RLlO was designed and developed for the National Aeronautics and Space Administration's Saturn S-IV azld Centaur space vehicles. A technique new to telemetry is discussed which promises to alleviate an enigma facing the telemetry engineer : How to adequately transmit the avalanche of vibration and other wideband data desired in the development phase of large missiles and launch vehicles. The data channels are stacked in the frequency spectrum as single sideband subcarriers which frequency modulate the RF carrier. The system design utilizes to advantage the statistical properties of vibration data to achieve maximum data transmission efficiency from the available RF carrier deviation. However, in contrast to proposed statistical predigestion techniques, the data is transmitted in raw form. A thesis presented to the faculty of the Fletcher School of Law and Diplomacy. In partial fulfillment of the requirements for the Degree of Doctor of Philosophy.; This document is only the abstract of the thesis.; Document includes biographical note and table of contents.; aArchive copy is a photocopy. A three-foot high Instrument tional Business Machines Corporation will be launched into orbit with a huge Saturn second stage
later this month in a crucial test for the Apollo lunar program. Abstract to "A thesis submitted to the faculty of Purdue University fo Gary Marshall Richetto in partial fulfillment of the requirements for the degree of Doctor of Philosophy, January 1969".; Handwritten note on front page: Return to Internal Communication, Room 223, 4202. ABSTRACT: Discusses intensive ground qualification testing program for S-IV stage. According to an abstract found on the page following the title page, this paper includes "one possible conceptual definition of an early Apollo Logistics Support Systems (ALSS) is presented and various payloads for the system are briefly discussed. " It also discusses the Lunar Mobile Laboratory (MOLAB) and other considerations for a lunar scientific mission. According to the abstract, this paper discusses the need for a uniform design approach throughout the aerospace industry for space vehicle structural vibrations in order to keep pace with improvements in environment definition and testing. According to the foreword found on page i, this document includes instructions on "procedures, methods and practices...necessary for the effective management of a program documentation system." According to the foreword, "This paper presents the results of a twelve-week mission and systems analysis of a combined Jupiter orbiter/solar probe mission utilizing the Saturn V launch vehicle." According to the introduction found on page ii, this document was created to detail the "MSFC segment of the total Apollo Management process and to describe the methodologies and techniques currently being implemented." According to the preface, "This handbook provides KSC management personnel with general information relative to the Apollo-Saturn program. Emphasis is placed on Saturn launch facilities and related support equipment. Saturn vehicle parameters are included for general information. According to the purpose found in section 1.1, "Volume I provides a guide for the preparation of specifications for existing equipment in the Apollo/Saturn Program." According to the summary found on page 1, this document "presents a brief and concise description of the AS-204/LM-1 Apollo Saturn Space Vehicle." The information within the document allows readers to follow the timeline of the space vehicle's lift-off and journey to space. According to the table of contents, this volume of appendices contain various charts, graphs, and diagrams related to the S-IC stage data, instrument unit data, and vehicle data. Address by Dr. George E. Mueller, Associate Administrator for Manned Space Flight, National Aeronautics and Space Administration before the Ninth National Conference of United Press International Editors and Publishers, October 8, 1968. Address by Dr. George E. Mueller, Associate Administrator for Manned Space Flight, National Aeronautics and Space Administration; Joint AIAA/CASI Meeting, Montreal, Canada, July 8, 1968. AS DELIVERED.; Includes charts. Address from General O'Conner to the Rotery Club bringing them up to date on organizational developments inside the George C. Marshall Center. Addresses improving spacecraft safety by resolving various known dynamic problems. Aerospace Workshop, University of Hawaii.; Includes references to slides. Aerospace Workshop. University of Hawaii.; Includes references to slides. AIAA Second Annual Meeting, San Francisco, California. Discusses the fabrication process of the Saturn S-IC booster. An article describing Huntsville's role in various space related projects. An article regarding Doctor Kurt Debris, director of NASA's Kennedy Space Center. An article which comments on the increasing interest in science and education due to the greater understanding of space. An entire newspaper containing a number of articles both related and not related to the Saturn program. An organizational chart directory. An outline of an interview with Wernher von Braun. Analysis of the stability and dynamic load environment of a launch vehicle resulting from atmospheric disturbances is a very complex problem. To determine the dynamic load environment of the vehicle requires an adequate description of the wind field, vehicle dynamics and control system. The essential of such a study, namely methods of analysis, wind field specification and representative vehicle response parameters for evaluation, are of equal importance. This paper is concerned with the mathematical foundations of the vehicle model and method of analysis. Appears to be a rough dfraft with editorial comments and revision notes. Includes references to figures and tables.; Page 31 is missing. Pages 37 through 44 do not exist; there is a note about this on page 36. Page 67 also does not exist. April 1, 1968.; Stamped on first page is From the Archives of Frederick I. Ordway, III. Archive copy is a photocopy. Archive copy is a photocopy.; Includes memorandum and information from George E. Mueller, Associate Administrator for Manned Space Flight. Letter contains handwritten editing and notes. Archive copy is a photocopy.; The purpose of these writings is to compile in one volume the basic elements of thermodynamics and gas dynamics which are useful in the evaluation of thrust chamber performance. It is presumed that the reader will have had an elementary course in thermodynamics and gas dynamics. The discussion of topics useful in evaluating thrust chamber performance is, of necessity, limited to these physical effects amenable to other areas that are as yet in the research stage of development. The author would like to take this opportunity to express his gratitude to Mr. G. S. Gill for many stimulating discussions on this subject. Thanks are due to Mr. D. J. Kuyper for permission to utilize his discussion on elastic-plastic strain and its application to nozzle throat area change. Finally, the author wishes to express his gratitude to his wife, Alice, who typed the bulk of the manuscript. Archive copy is a poor photocopy. Prepared for presentation at Deutsche Gesellschaft fur Raketentechnik und Raumfahrt. (German Society for Rocket Technology and Astronautics). Given by E. Harpoothian, Chief Engineer, Structures Department, Development Engineering.; Tanks for cryogenic fluids, as used in the Saturn space vehicles, have reached an advanced stage of design and development. Many of the structural features of the NASA/Douglas Saturn tanks, fabricated of 2014-T6 aluminum alloy, were first developed for the booster of the Thor ballistic missile, which later found extensive use in putting space vehicles into orbit. There is a mutual dependence of important factors related to design concepts, selection of materials, processing techniques, and fabrication methods. It is shown that this mutual dependence must be considered if a successful vehicle is to emerge from design and development. Details of vehicle structure, provision for insulation, and manufacturing methods are presented. Criteria for the selection of materials is shown to be dependent on strength, ductility, weldability, toughness, fabricability, behavior at cryogenic temperatures, and on manufacturing methods and inspection techniques. Archive copy is a poor photocopy. Cannot read. Archive copy is a poor photocopy. Unable to read. Archive copy is a poor photocopy.; Article is from Defense Industry Bulletin, October 1959, pages 21 to 24. Archive copy is a poor photocopy.; Handwritten on the first page is "10/25/67".; Includes a letter dated Nov. 6, 1968 to Mr. Christensen from William D. Putnam. Archive copy is a poor photocopy.; Handwritten in ink is: Ref: Goddard Patents (See D. Akens for final draft of letter). Article aimed at improving the NASA's ability to complete its projects." Article containing diagrams about the pumping and boiling process of water. Article covering the development of cryogenic pumps. Article detailing the different aspects of the Launch Complex 34 facilities. Article discussing money-resources and the budget. Article explores the outer layer of the Saturn S-II along side its benefits and complications. Contains poorly rendered images displaying the process. Article makes references to a film. Centers around the idea that testing space vehicles extensively before launch is cost control. Article noted in the table of contents : Guidelines for administrators by William Sheil. Pages 6 and 7. Article refers to photographs, providing context to what is shown in them with formulas and measurements. As this paper is being written, the Saturn I flight test program includes five flights launched between October, 1961 and January, 1964. All five fiights were complete successes, both in achieving all major test missions and in obtaining an unprecedented volume of system performance data for flight analysis. Aspects of Earth-to-orbit delivery are discussed and a cost analysis of the logistic operation and the cost of orbital operations are presented. Probabilities of success of orbital delivery and the operational and economic aspects of establishing large orbital installations and maintaining a large transportation volume in the 1975/85 time period are compared for the two cases using a large number of Saturn V versus a smaller number of 1-stage chemical Post-Saturn launch vehicles. Performance parameters of chemical, chemonuclear and nuclear launch vehicles are compared. The concept of a blunt launch vehicle configuration referred to as NEXUS is presented in detail. Applications of this configuration to chemonuclear propulsion and to a 50 ft diameter version of Saturn V with recoverable first stage are discussed. ATOLL was developed to fulfill the requirements for a common computer language that could be used by the test engineers for launch and factory checkout. "ATOLL" is the abbreviated name for Acceptance, Test, Or Launch Language. Because of the increased reliability required of rocket systems in their more recently assigned missions, previously acceptable design features must be reappraised ad refined. In the region of rocket engine system stability, the probles is centered in two areas, the combustor and the propellant feed system The principal interest of this paper lies in the coupling that occurs between the feed system and combustion dynamics, often termed a "buzzing" instability then the dymics are characterized by periodic pressure oscillations in the range of 200 to 1000 cps appearing in the combustion chamber and' the feed system. Bibliography containing space crews, space flights, satilites, cryogenic propellants, propaganda and the USSR. Bibliography of technical reports from 1957-1963 Brazing as a technique for joining metal parts has been utilized for centuries. Industry, however, has only begun to use it on a wide scale in the last twenty years. The rapid growth of brazing has been a result of consumer and military demands Tor products of lighter weight, less expense, and higher performance. Today, brazing is one of the most widely used fabrication techniques in the production of liquid rockets, gas turbines, refrigerator and other types of heat exchangers, automobile parts, vacuum tubes, and many nuclear products. By J. Reynolds Duncan, Jr., Aerospace Engineer, NASA Marshall Space Flight Center, Huntsville, Alabama. AIAA 7th Aerospace Sciences Meeting, New York City, New York, January 20 - 22, 1969. Case histories of seven typical failures in large liquid propelled rocket engines components have been prepared. Quite simple to complex investigations are presented covering a variety of failure modes in a variety of materials. Included are successful solutions to the failure problems investigated.; Archive copy is a poor photocopy. Chart No. 1 Rocketdyne master approved by S. K. Hoffman, President (Vice President, North American Aviation, Inc.,).; Chart No. 6.1 Engineering Field Laboratories approved by R. J. Lodge, Director.; Chart No. 6.1.1 Santa Susana Field Laboratory, approved by D. M. Carpenter, Manager.; Chart No. 6.1.2 Field Laboratories Nevada Field Laboratory approved by G. J. Wunderlin, Manager.; Chart No. 6.1.3 Edwards Field Laboratory approved by F. F. Twight, Manager.; Chart No. 6.6 Engineering Administration approved by P. J. Kanne, manager.; Chart No. 12 Solid Rocket Division approved by T. E. Myers. Comment draft. Text drafted by Science and Technology Division, Library of Congress. Configuration management: Definition, requirements, organization, policy and procedure documents, contractual documents. Considerations for improvement in the reliability of the Saturn engine gimbal servosystems are briefly covered. The Saturn I servovalves operate with increased electrical input power. The Saturn V vehicle stages will use mechanical feedback actuators with increased electrical input power, larger orifices and nozzle sizes, larger torque motor wire size, and greater spool driving forces. 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, & -C." Copy No. 026. Ger-10866. Correspondance between Edmund F. O'Conner and David L. Christianson in which Edmund encloses three documents to David and expresses his gratitude for David's work on the history of the Saturn V program. Correspondance between Professor Logsdon and Welsh regarding Logsdon quoting Wernher von Braun's memorandum. Correspondance between the President and Hugh L. Dryden regarding administrative limitations of the President's power. Correspondence letter detailing Mueller's concerns regarding potential issues in the design of the Saturn stages. Corrosion problems associated with space vehicles, in general, are discussed as contrasted to those problems experienced with structures in an earth atmosphere. Primary emphasis is placed on structural alloys in this discussion, although some corrosion failures experienced in various mechanical components are described. General corrosion prevention measures are indicated, and solutions to specific corrosion failures described. Major failures experienced have been attributed to stress corrosion cracking, rather than general or galvanic type corrosion. Most such failures have occurred with only five different materials: three aluminum alloys - 7075-T6, 7079-T6, and 2024-T6; and two precipitation hardening stainless steels - 17-7PH and AM 355. Corrective actions were different in each case, but involved either a complete change to another material, a change to a different temper of the same alloy, or a modification of the heat treatment and/or general processing techniques. General conclusions are that the types of failures described could be avoided by: a more suitable selection of alloys in the initial design, a realistic review of the environments that could be encountered in the service lifetime of the component, lowering stresses, improving process controls, and effecting better familiarization of design personnel with the with the overall stress corrosion problem in an effort to reduce human error.; Preprint 18e.; Materials for re-entry and spacecraft systems - spacecraft materials.; Materials Conference, Philadelphia, Pennsylvania, March 31 - April 4, 1968. Cover has: P. D. Castenholz and H. K. Griggs, Advanced Systems, Advanced Projects Department. D. W. Hege, Manager, Advanced Projects. Paper regarding the importance of propulsion technology and the future missions that would require advancements in that field. Cryogenic propellant rocket engine hardware and the related test facilities will be described. Methods used for selection of alloys for liquid oxygen and liquid hydrogen service will be discussed. Unique equipment and welding procedures are reviewed with emphasis on welding problems and their solutions to assure reliable hardware and facilities. Examples of specific welding procedures and methods of quality assurance will be given for joining application ranging in size from .001" to 11" thick sections. Describes different aspect of the Fault Simulation for Saturn computer design. Describes the F-1 engine design and components. Describes the purpose and goes of the George C. Marshall Space Flight Center. Instrumental development branch. Describes the SIV vehicle and its components. Presented at: IRE International Convention. Describes the structure and function of each part of the NASA Lunar Module Description of a photograph of a rocket static test firing. Description of an 8 x 10 inch black and white photograph. Description of the Transtel without accompanying photograph. Design review is becoming a basic requirement during the design and development of military systems. The main purpose of the design review is to increase the system's inherent and operational reliability. The major portion of this paper is the result of reliability's effort to comply with Paragraph 3.6 of NPC 250-1 Reliability Program Provisions for Space Contractors. The design review to be discussed is a reliability circuit design review with emphasis placed on what should be reviewed and the review techniques employed. The basic circuit design review prerequisites, component parts and their ratings, are discussed at the beginning of this paper. The remainder deals with the organization and reviewing of circuits. The review items include worst-case circuit performance, component applications, failure mode analysis, noise rejection, electrical stress, and the determination of component temperatures. Many examples are included to illustrate how each item was accomplished. This paper is intended not only to give the reliability analyst cognizance of basic design problems and troublesome circuits, but also, to aid him in formulating a design review program. Details contracts for upper stages of Saturn IV and Saturn V and includes illustrative appendixes. Archive copy is a photocopy. Diagram displaying the internal rooms, pieces and functions of the Saturn V as well as the space-suits of the astronauts. Diagram displaying the launch escape system flight separation in progress. Diagram explaining the process of a lunar mission from liftoff to recovery. Diagram that displays the Saturn V rocket with a page beneath detailing the function of each stage. Dieter Grau interviewed on failure analysis and management of Saturn program. Both sides of tape. Digesu worked in the Astrionics Division of MSFC. This paper was presented at the AIAA Guidance & Control Conference, Massachusetts Institute of Technology, Cambridge, Massachusetts, August 12-14, 1963. Digital computer simulation of the Saturn I Instrument Unit electrical networks was accomplished using the Discrete Network Simulation programs. The schematics were analyzed and a logic model prepared which consisted of a series of Boolean equations. The test procedures, which are written in the Acceptance, Test, or Launch Language (ATOLL), consist of a sequential set of computer instructions for the RCA llOA checkout computer to control the operation of the electrical networks. The procedures also contain the predicted results for each operation. The driving functions for the simulation of the model are generated from the ATOLL test tape by the Input Generator Program. The time sequenced operation of the networks is indicatedby the output from the simulation program in addition to the number of times each component in the system changes state. The results of the simulation are compared to the test procedure predictions on the ATOLL tape by the Comparator Program and any differences are listed. The Comparator Program also lists any component which did not change state at least once. Directory of different sections with descriptions underneath. Discusses the importance of redundancy as a safety measure in electronic systems. Document detailing the history of the saturn project between April, 1957 through November, 1962. Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points. Document that discusses the importance of reliability in engineering. Douglas Aircraft Company Report DAC-56445, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during August and September 1966. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-101. Douglas Aircraft Company Report DAC-56533, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during January, February, and March 1967. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-01.; Prepared for National Aeronautics and Space Administration under NASA contract NAS7-101.; Approved by A. P. O'Neal, Director, Saturn Development Engineering. Douglas Paper No. 4396.; Prepared by Ludwig Roth, Director, Saturn/Apollo Program Extension, Douglas Aircraft Company.; Presented to 16th Annual Conference of the Hermann Oberth Society. Discusses the role of the Apollo rocket after the Apollo program has concluded. Draft of working paper. Typed with handwritten notes (title and author) and pages. Copy in MSFC files noted on first page. Draft script for quarterly report: July through September, 1965. Drawn by Don Sprague at the Huntsville Engineering section of Boeing. During cryogenic weigh system operation, hydrogen when combined with oxygen can create an unsafe condition. Therefore the concentration of the residual oxygen and hydrogen from leaks in the cryogenic weigh environmental bags must be known at all times during the cryogenic weigh. Hydrogen and oxygen detectors will provide the optimum method for maintaining safe conditions. Hydrogen properties and safe mixtures are reviewed. The method selected to analyze the oxygen content is discussed. The selection, development, and testing of a hydrogen detector system is examined. During long coast periods of zero-gravity, storage vessels for the cryogenic liquids proposed for use in some power transmission systems undergo random distribution of the liquid and vapor phases therein. Thus, when heat flow into the vessel causes the vessel pressure to build-up requiring venting to maintain a safe value, the likelihood of venting the valuable liquid phase, as well as the vapor, results. To preclude this eventuality, various devices for separating the liquid and vapor phases and venting just the vapor have been studied and carried into the experimentation stages. During the development of the RL-10 and J-2 engines, many problems were encountered. Solutions to the significant problems are contained. A description of these LOX-Hydrogen engines, outlining the unique features of each will be given. Performance parameters for both engine systems are tabulated. Specific applications to various stages are shown. Essay detailing potential candidates for potential interviews. Essay detailing the relationship between men and machines." Essay that focuses on the achievements of the Grumman Aerospace Corporation. Excerpt from G.E. Challenge , Fall (Sept.) 1968, pages 13 to 25. Excerpt of contracts MSFC 1962, pages 76-79. Exerpt from George E. Mueller giving a statement to Congress. Film script for the Saturn Quarterly Film Report - April through June, 1964. Film script for the Saturn Quarterly Film Report - April through June, 1965. Film script for the Saturn Quarterly Film Report - January through March, 1964. Film script for the Saturn Quarterly Film Report - January through March, 1965. Film script for the Saturn Quarterly Film Report - October through December, 1964. Film script for the Saturn Quarterly Film Report - October through December, 1965. Film script reporting on how the Saturn 1 will be used and what its take-off process will look like Film script reporting on the construction of the Saturn 1 Film script reporting on the testing of the Saturn 1 Finding the turbopump arrangement which is best suited for a given rocket engine - space travel applications - constitutes an important task. The arrangement depends upon a large variety of different factors, such as, the engine cycle, weight, the liquids to be pumped, the cavitation performance, the bearings and their lubrication, the seals and the turbine. In this report these factors and their influence on the turbopump configuration are discussed. It is shown that three of them: weight, propellants to be pumped and obtainable suction performance have the largest influence on the selection of the turbopump. A systematic approach is outlines for the design process, which allows to arrive at a turbopump arrangement best suited for a given application. Focuses on the construction and future use of the Apollo space telescope. The components described in this paper except for those listed otherwise were designed by the Space Support Division of Sperry Rand Corporation to specifications established by NASA's Marshall Space Flight Center in Huntsville, Alabama. Appreciation is extended to MSFC for permission to publish this paper and for data and help provided for its preparation. Folder of information. Following is text of Douglas release on successful first firing of clustered P&W RL10 engines. Occurred at 11:12 A.M. PDT, August 17. Santa Monica, California.; "Sacramento, Calif,--Man's effort to reach the moon moved nearer reality today with the successful first firing here of the six liquid oxygen-liquid hydrogen fueled engines of the Saturn S-IV. For presentation at the Aerospace Industries Association of America (AIA) Manufacturing Engineering Committee Meeting. Discusses the role the NASA Engineering Laboratory has had on NASA projects in the form of vehicles and smaller projects.
