Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 18.
Saturn Project (U.S.)
Project Apollo (U.S.)
Saturn launch vehicles--Testing
Saturn 5 launch vehicles
Apollo spacecraft
Tests
The document is Volume 1, Section 18 of a list of Saturn V launch tests including but not limited to test titles, test numbers, test objectives, and test descriptions related to AS-502.
John F. Kennedy Space Center
University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
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Reports
Text
Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 19.
The document is Volume 1, Section 19 of a list of Saturn V launch tests including but not limited to test titles, test numbers, test objectives, and test descriptions related to AS-502.
Catalog of launch vehicle tests Saturn V : Apollo/Saturn 502 : Volume 1, Section 20.
The document is Volume 1, Section 20 of a list of Saturn V launch tests including but not limited to test titles, test numbers, test objectives, and test descriptions related to AS-502.
Convective Energy Transport in Stellar Atmospheres: A Convective Cell Model.
Saturn project
Transport theory
Convection
Stellar atmospheres
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.
Ulrich, Roger K.
Essays
"Crew Briefing : Instrument Unit Stage Presentation".
Saturn launch vehicles
Spacecraft control
Spacecraft guidance
Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
International Business Machines Corporation
Petrone, Rocco A.
Teir, William
Presentations
"Film script for Saturn I/IB quarterly film report no. 15."
Saturn launch vehicles--Design and construction
Saturn 1 launch vehicles
Saturn 1B launch vehicles
Film scripts
Unclassified film script of the Saturn I/IB Quarterly Film Report covering January, February, March, 1963. There are handwritten notes and edits throughout the document.
Conover-Mast Publications, Inc.
"Film script for Saturn I/IB quarterly film report no. 16."
Unclassified film script of the Saturn I/IB Quarterly Film Report covering April, May, June, 1963. There are handwritten notes and edits throughout the document.
"Film script for Saturn quarterly film report no. 18."
Unclassified film script of the Saturn I/IB Quarterly Film Report covering October, November, December, 1963. A handwritten note at the top of the title page lables this copy as the "Final Draft".
"U.S. Aerospace Program: missions and projects as of January 1, 1966."
Astronautics--United States
NASA space programs
Space vehicles
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.
Still Image
Pictures
"Use of tank mounted booster pumps for providing NPSH to turbopumps operating in a radiation environment."
Liquid hydrogen
Cavitation
Cavitation flow
Turbine pumps
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.
DiStefano, John F.
Borg-Warner Corporation. Pesco Products Division
Apollo project
Outer space--Exploration
Moon--Exploration
Lunar exploration
Space flight
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.
Gordon, T. J. [Gordon, T. J. (Theodore Jay)]
Douglas Aircraft Company. Missile and Space Systems Division. Space Systems Center
Organization charts of ABMA during 1957-1960.
Organization charts
Includes letter to Mr. David Christensen, University of Alabama Research Institute.
United States. Army Ballistic Missile Agency
Correspondances
"Vibration and acoustic environment characteristics of the Saturn V launch vehicle."
Saturn launch vehicles--Vibration
Saturn launch vehicles--Acoustic engineering
Vibration
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
Beck, Clark J.
Caba, Donald W.
Graphs
George C. Marshall Space Flight Center--Visual aids
Slides
Indexes
This document includes revisions. There are missing pages from page 237-238. This reference document catalogues all MSFC oriented visual aids filed in the Visual Aids Library of Marshall Space Flight Center. These visual aids are updated by the Graphic Engineering & Models Branch, Industrial Operations Program Management Information Office, and the Research and Development Operations Management Office. The purpose of the Visual Aids Library is to provide management data visuals in the form of slides (3 X 4 and 2 X 2), or black and white prints, to MSFC offices and laboratories, and other centers, who have a valid requirement. The visual aids are issued on a loan basis in order to obtain as wide a use for each visual and to assure that the latest revisions are incorporated in the issued item. Visuals may be ordered from the Visual Aids Library, located on the 10th floor of building 4200 (Phone 876-7237, 876-6960, 876-0983). In addition to the visuals published in this book, photographs from prime contractors are available from Industrial Operations, Program Management Information Office, Room 621, building 4201. Visuals with erroneous or obsolete information should be brought to the attention of the Visual Aids Library, preferably in writing, so that corrections can be made immediately. This publication will be kept current through distribution of pages of new visuals and notification will be made on obsolete visuals so they may be crossed out in the catalogue. Comments and suggestions concerning this publication will be greatly appreciated. Changes in the distribution lists should be directed to Mr. Gordon 0. Willhite, or Mrs. Opal Tabor, Visual Aids Library, MS-G.
George C. Marshall Space Flight Center. Management Services Office
"Von Braun's move ended Moon-Bug NASA dispute: rocket pioneer had favored earth-orbital rendezvous plan."
Moon
Silcock, Bryan
Newspapers
Vonbraumoveende_072910160005.pdf SAME ARTICLE LESS DAMAGED DOC SCANNED IN BLACK AND WHITE IS TITLED VonBraumoveende_052410123817
"Welding cryogenic materials for aerospace applications."
Liquid propellant rockets--Fuel tanks--Design and construction
Welding
Cryogenic tanks
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.
Photographs
"Welding for aerospace application : a panel discussion."
Aerospace industries
Standards
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.
Wilson, W. A.
Transcriptions
Space race
Space flight to the moon
Astronautics--Soviet Union
Interview
Partial article discussing the United States' victories in the space-race over Russia.
General Electric Company. Missile and Space Division
Challenge G. E.
Interviews
"Where are we going in space management."
Astronautics--Systems engineering
Project 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
Reed, Joseph H.
"Why internal insulation for the Saturn S-IV liquid hydrogen tank?."
Liquid propellant rockets
Propellant tanks
Fuel tanks--Linings
Saturn S-4 stage
Prepared for presentation at the Cryogenic Engineering Conference, Los Angeles, California, August 14-16, 1962.; There is no page 8.
Herstine, Glen L.