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Film script for Saturn C-1/C-1B quarterly film report no. 13 (covering July, August, September, 1962).
Film script reporting on how the Saturn 1 will be used and what its take-off process will look like -
F-1 engine photograph.
8 x 10 inch black and white photograph. Engine parts are labeled. -
DX priority: memorandum.
Memorandum discussing the priorization of various nlunar landing vehicle projects. -
Dr. von Braun's oral history interview transcript - Kennedy Library: memorandum.
This memorandum references the signed copies of Dr. von Braun's oral history interview for the John F. Kennedy Library. -
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.
The first page contains a typed routing slip. A list of Wernher von Braun's meetings with President Kennedy, the Vice President and members of their immediate staff. -
Douglas Aircraft news release.
ABSTRACT: Discusses intensive ground qualification testing program for S-IV stage. -
Douglas Aircraft news release.
ABSTRACT: Discusses intensive ground qualification testing program for S-IV stage. -
Double seal insulation [drawing] photograph.
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. -
Directory Chart : NASA/MSFC Manager's Office.
Organizational chart of NASA/MSFC manager's office. -
Differences of configuration in successive Saturn IB and Saturn V vehicles- case 330.
Includes memorandum for file. Configuration matrices reflecting present program status of differences in Saturn IB and Saturn V flight hardware on a mission to mission basis have been prepared. The attached matrices are arranged to show differences in major subsystems (Structures, Propulsion, Instrumentation and Range Safety, and Electrical) for each stage. The reason for the configuration difference and the mission effectivity are included.; DMD, 2031-SGE-eas, GRH; Includes "Recommendation for announcement and distribution of Bellcomm Report". -
Development of LOX/RP-1 engines for Saturn/Apollo launch vehicles.
The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, may problems were encountered. Mehtods of solving the combustion instability problem are discussed.; AIAA 4th Propulsion Joint Specialist Conference, Cleveland, Ohio, June 10-14, 1968.; Also available on NASA Technical Reports Server (NTRS) as unclassified. Can be ordered. Also on AIAA. -
Contractors over $700,000 that made contribution to Saturn.
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. -
Contract let for $8 million for work relating to upper stages of Saturn rockets : news release.
News release describing Saturn V contracts for various components, the companies awarded the contracts, and contract amounts. -
Contact points within the NASA for exchange of information on lunar program matters.
Memorandum to Colonel J. W. O'Neill, Plans & Operations, Air Force Ballistic Missile Div. (ARDC).; Archive copy is a poor reproduction. -
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.
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. -
Comments on SA-5 mission.
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. -
Combustion Oscillations in F-1 Engine.
The set of documents includes an introductory letter written by D. Brainerd Holmes and Tischler's report with the subject "F-1 Combustion Instability Report for Associate Administrator; Period March-April, 1963". -
A "Think Clean" training program.
This paper outlines steps involved in preparing and presenting an instruction course on clean rooms. The training area, personnel, equipment, and program outline will be described. A summary of the results obtained over the first year of operation will be presented. -
Convective Energy Transport in Stellar Atmospheres: A Convective Cell Model.
One of the Orange Aid Preprint Series in Nuclear Astrophysics, September 1968.; Supported in part by the National Science Foundation [GP-7976], the Office of Naval Research [Nonr-220(47)]. ; ABSTRACT: The motion in a convectively unstable region is expanded into an ensemble of convective cells. Each of these cells interacts with the surrounding medium according to the semiempirical model proposed by Turner (1963 ). Possible detailed models of the flow patterns within each cell are presented. The radius and velocity of these cells are given as functions of distance moved. The convective flux and rms velocity are given as averages over the ensemble of cells. As in the standard mixing length theory the principle uncertainty remains the average initial radius of the cells. -
Convective Energy Transport in Stellar Atmospheres: A Convective Cell Model.
One of the Orange Aid Preprint Series in Nuclear Astrophysics, September 1968.; Supported in part by the National Science Foundation [GP-7976], the Office of Naval Research [Nonr-220(47)]. ; ABSTRACT: The motion in a convectively unstable region is expanded into an ensemble of convective cells. Each of these cells interacts with the surrounding medium according to the semiempirical model proposed by Turner (1963 ). Possible detailed models of the flow patterns within each cell are presented. The radius and velocity of these cells are given as functions of distance moved. The convective flux and rms velocity are given as averages over the ensemble of cells. As in the standard mixing length theory the principle uncertainty remains the average initial radius of the cells. -
"X-ray television inspection of aerospace weldments : Television x-ray image enlargement system for inspection."
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. -
"Why internal insulation for the Saturn S-IV liquid hydrogen tank?."
Prepared for presentation at the Cryogenic Engineering Conference, Los Angeles, California, August 14-16, 1962.; There is no page 8. -
"Where are we going in space management."
Presented to the First Space Congress, Cocoa Beach, Florida, April 21, 1964 by Joseph H. Reed, Chief, Management Analysis Office, Executive Staff, Marshall Space Flight Center at the request of the Associate Administrator for Manned Space Flight, NASA -
"Welding for aerospace application : a panel discussion."
Original is a photocopy; W. A. Wilson, Chairman; Russell Meredith, North American Aviation; Robert Hackman, Linde Company; Frank Wallace, Pratt-Whitney Aircraft; P.G. Parks, NASA, MSFC; G. O. Hoglund, Aluminum Company of America. -
"Welding cryogenic materials for aerospace applications."
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. -
"Welcome back planned for 'Gum Drop' crew."
A news article detailing the festivities planned upon the return of nine astronauts returning from a 10-day mission. -
"Welcome back planned for 'Gum drop' crew."
News article detailing the planned 'Welcome back' events surrounding the resturn of the Apollo 9 crew. -
"We're winning the race with Russia."
Partial article discussing the United States' victories in the space-race over Russia. -
"Vol. IV 3rd edition Management Information."
This document contains copies of management charts and photographs maintained in the Management Information Office of the Executive Staff on Advanced Program and Research and Technology Areas. -
"Vibration and acoustic environment characteristics of the Saturn V launch vehicle."
This paper presents representative examples of vibration and acoustic data from flights of the Saturn V launch vehicle and static firings of Saturn V launch vehicle stages. The purpose of the paper is to provide vibration and acoustic environment characteristics which are pertinent to the design of launch vehicles -
"Uses of Saturn."
Saturn and Apollo hardware will not have realized their ultimate potential for space exploration after the project lunar landing is complete. To accomplish the Apollo lunar landing program, an immense backlog of technology, facilities, and booster capability will have been built up, and we believe proper utilization of this resource will fill the needs for planetary, lunar and earth orbital space exploration for years to come. -
"Use of tank mounted booster pumps for providing NPSH to turbopumps operating in a radiation environment."
This paper outlines the results of a test program which was planned to demonstrate the feasibility of using a tank mounted, all-inducer, high speed liquid hydrogen booster pump to provide NPSH for the turbo pump in a reactor-powered vehicle. The cavitation problem associated with pumpoing liquid hydrogen, when used as a propellant, is further aggravated by localized heating caused by radiation from the reactor. -
"University and research institute contracts awarded by MSFC."
This is a list of contract numbers, contractor, subject and RNT contact. -
"United Aircraft Quarterly Bee-hive:" Spring, 1962: Volume XXXVII, Number 2.
A book containing various articles surrounding the activities and achievements of the Saturn program up to Spring, 1962. -
"United Aircraft Quarterly Bee-hive:" January 1962, Volume XXXVII, Number 1.
A book containing various articles surrounding the activities and achievements of the Saturn program up to January, 1962. -
"Ultra high strength composite materials."
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. -
"U.S. Aerospace Program: missions and projects as of January 1, 1966."
The document contains four charts labeled "Investigation", "Exploration", "Utilization", and "Control". Each chart is organized chronologically, contains drawings of U.S. Aerospace Program Projects, and incudes written descriptions of each project. -
"Trends in procurement" by Garland Buckner.
Speech delivered by Garland G. Buckner to the National Contract Management Association, Huntsville Chapter. Discusses the outdated procurement process, how its changing and how to track the trends of how its changing. -
"Transportation of Douglas Saturn S-IVB stages."
Presented to the American Society of Civil Engineers by R. W. Prentice, manager, Saturn Logistics Support, Douglas Aircraft Company Inc., Missile & Space Systems Division, Space Systems Center, Huntington Beach, California. This paper describes the significant events and equipment associated with transporting the Douglas Aircraft Company, Inc., built Saturn S-IVB stage from stage fabrication at Huntington Beach, California, to the Sacramento Test Center and to the Kennedy Space Center. Descriptions and illustrations of the transportation vehicles and major ground support and instrumentation equipment are presented for a more comprehensive understanding of the transportation problem.