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The "Apollo/Saturn Data Handbook."
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. -
Telegraphic message containing an Apollo Program Flash Report.
This message for the Apollo Program Director contains a report of the Apollo launch vehicles, problem that occurred, and actions required. The photocopy is difficult to read. -
Telegraphic message containing an Apollo Program Flash Report.
This message for the Apollo Program Director contains a report of the Apollo launch vehicles, problem that occurred, and actions required. The photocopy is difficult to read. -
Technical information summary of the Apollo Saturn 1B flight vehicle.
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. -
Saturn V management information : August 1964 : Volume VI.
This document contains copies of management charts maintained in the Managerial Data Center of the executive Staff on the Saturn V project. To facilitate use of this document, all Saturn V classified data has been removed and will be published in Volume XI. A list of these charts are shown on the "Table of Contents". Information on other MSFC activities will be published in separate volumes as indicated on the "Schedule for Publication of Data Bank Charts" contained in this volume. -
Saturn V history team at the Apollo 10 launch.
Shown left to right: David Christensen, Melvin Kranzberg, Irving B. Holley, Jr., Rudolf Hermann, and Fred Ordway. -
Saturn Launch Vehicles Astrionics System Handbook.
Includes change pages. Contract NAS8-14000. Second revised edition. V66-15610. NASA-CR71607. The introduction notes, "This second revised edition of the Astrionics System Handbook has been developed under the direction and overall supervision of Dr. Rudolf Decher of the Astrionics Systems Engineering Office. This description of the Saturn Astrionics System has been generated by personnel of the Astrionics Laboratory, the staff of the Astrionics Systems Engineering Office, and by personnel of the International Business Machines Corporation working under Contract NAS8- 14000. The handbook will be updated and expanded as it becomes necessary due to changes or refinements in the system concept and hardware. Sections not contained in the first release of this document will be made available within three months." Signed by Ludie G. Richard, Chief, Systems Engineering Office, Astrionics Laboratory. The document is missing pages in the following locations: Chapters 8, 9, 12. Sections 15.2, 15.3, 15.4-1 thru 15.4-16, 15.5-1 thru 15.5-2, 15.5-5 thru 15.5-8. -
Saturn Launch Vehicles Astrionics System Handbook, 2nd revised edition.
This updated edition of the Astrionics System Handbook instructs, "The enclosed pages change, delete, or supplement the information in the Astrionics System Handbook (1 August 1965). Insert these pages and destroy the pages they replace." -
Saturn AS-501 evaluation bulletin No. 1, November 14, 1967.
The findings herein are the results of the combined evaluation efforts of the various Laboratories of Research and Development Operations at MFSC, The Boeing Company, North American Rockwell/Space Division, Douglas Aircraft Company, International Business Machines, and Rocketdyne. -
Saturn and lunar flight.
Speech by K.K. Dannenberg at American Society of Civil Engineers, Huntsville, November 2.; Projectionist's copy (photocopy) - slide numbers are included. -
S-IVB cutaway and J-2 engine."
8 x 10 inch black and white diagram of the JII engine and the Saturn IV. -
Press Release : S-IC simulator--Immediate release.
Huntsville, Ala. -- NASA Marshall Space Flight Center engineers and scientists will soon begin using a giant Saturn V booster simulator in making various tests of equipment and facilities here and at Michoud Operations, Mississippi Test Operations and Cape Kennedy. -
Preservation, shipment & recovery of the Saturn booster.
The purpose of this report is to present the shipping and recovery procedures for the Saturn booster. -
Marshall Space Flight Center Space Day 1961 program.
The program includes "Marshall Center Highlights" from the Center's first year, a message from director Wernher von Braun, a photograph of the Space Queen and Princesses, and a guide to the Center's buildings. -
Final Apollo 11 Lunar Surface Operations Plan.
Prepared by the Lunar Surface Operations Office, Mission Operations Branch, Flight Crew Support Division. -
DX priority: memorandum.
Memorandum discussing the priorization of various nlunar landing vehicle projects. -
Draft of "Concepts of the Iterative Guidance Law for Saturn Launch Vehicles."
The summary notes, "In 1960, research work was begun to develop new guidance concepts for the Saturn space vehicles. [...] This paper presents the basics of the Iterative Guidance Law developed for Saturn launch vehicles to meet these new requirements of space age guidance. The development of the Iterative Guidance Law and the results and ideas presented in this paper are due primarily to Mr. Helmut J. Horn and his associates in the Dynamics Analysis and Flight Mechanics Division of the Aero-Astrodynamics Laboratory." Marked "Research Review, OK" in the upper right corner of the first page. The document includes corrections and additions to the text in red pencil. -
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. -
Artist's Conception of the RL10-powered Saturn S-IV Stage.
This artist's rendering of the RL10-powered Saturn S-IV stage is depicted as heading toward deep space after separation from the booster. The drawing is accompanied with a brief description of the Saturn S-IV. -
Apollo 5 press kit.
For release Thursday P.M., January 11, 1968. -
Apollo 10/AS-505 mission chart.
The chart includes diagrams, mission statistics, crew, and notes. There is an additional copy in the David Christensen Collection. -
Apollo 10 press kit.
The press kit includes documentation on the Command and Service Module, Lunar Module, Saturn V launch vehicle, astronauts, and mission descriptions. Release No. 69-68. -
A Saturn rocket stage is loaded onto a barge on the Tennessee River.
The stage is being transported to the Mississippi Test Facility. -
A Saturn rocket stage is loaded onto a barge on the Tennessee River.
The stage is being transported to the Mississippi Test Facility. -
A Saturn rocket stage is loaded onto a barge on the Tennessee River.
The stage is being transported to the Mississippi Test Facility. -
A Saturn rocket stage is loaded onto a barge on the Tennessee River.
The stage is being transported to the Mississippi Test Facility. -
A Saturn rocket stage is loaded onto a barge on the Tennessee River.
The stage is being transported to the Mississippi Test Facility. -
"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 -
"This is Your Chrysler Saturn Story."
The document is a booklet created as part of the NASA/Chrysler Corporation Space Division manned flight awareness program. It discusses Chrysler's role in manufacturing and testing the Saturn and includes photographs and diagrams of Saturn stages, operations at Michoud, testing, and future missions. The section headings included in this booklet are "Chrysler and the Saturn," "Saturn at Michoud," "The Voyage of Saturn," "Saturn Firings," and "Saturn's Missions." -
"The toughest weld of all" S-II stage manufacturing.
Article explores the outer layer of the Saturn S-II along side its benefits and complications. Contains poorly rendered images displaying the process. -
"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 Saturn S-IVB stage has a requirement for orbiting around the earth for up to 4.5 hours with approximately 60 percent of its initial propellant remaining at the end of the coast (prior to restart) . Extensive analyses must be performed to insure that this requirement is met. Both the maximum and minimum heat transfer rates are important because the maximum rates affect the hydrogen boiloff losses and thus the initial propellant loading requirements. The minimum rates are important because the boil off gases are used to maintain a minimum axial thrust level by venting the gases continuously through aft facing nozzles. This provides for a settling of the propellant throughout the orbital coast and alleviates the need for periodically venting the tank under zero gravity. -
"The Saturn S-II."
The S-II is the second stage of NASA's Apollo moon-landing rocket - the giant Saturn V. The most powerful hydrogen-fueled booster under production, the S-II is destined for Apollo manned lunar missions and will help power three Americans to the moon. The S-II is being developed and manufactured at Seal Beach, Calif., by North American's Space and Information Systems Division, Downey, Calif., under the technical direction of NASA's Marshall Space Flight Center, Huntsville, Ala.