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"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. -
"The TV system for the Apollo telescope mount."
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. -
"Technical Information Summary Apollo 8 (AS-503) Apollo Saturn V Space Vehicle."
This document is prepared jointly by the Marshall Space Flight Center laboratories R-AERO-P, R-ASTR -S, and R-P&VE-VN . The document presents a brief and concise description of the AS-503 Apollo Saturn Space Vehicle. Where necessary, for clarification, additional related information has been included. It is not the intent of this document to completely define the Space Vehicle or its systems and subsystems in detail. The information presented herein, by text and sketches, describes launch preparation activities, launch facilities, and the space vehicle. This information permits the reader to follow the space vehicle sequence of events beginning a few hours prior to liftoff to its journey into space. -
"The uprated Saturn I - its growth potential & future role in space."
Remarks by Vaino J. Vehko, Director of Engineering, Chrysler Corporation Space Division at 30th Annual Meeting, Aviation/Space Writers Association, Las Vegas, Nevada -
"Test Laboratory monthly progress report" October.
Laboratory monthly progress report for the Saturn 1B program between dates October 1st through October 31st, 1967. Page 17 missing. -
"Test Laboratory monthly progress report" December.
Laboratory monthly progress report for the Saturn 1B program between dates December 1st through December 31st, 1967. -
"Test Laboratory monthly progress report" July.
Laboratory monthly progress report for the Saturn 1B program between dates July 1st through July 31st, 1967. -
"Test Laboratory monthly progress report" August.
Laboratory monthly progress report for the Saturn 1B program between dates August 1st through August 31st, 1967. -
"Test Laboratory monthly progress report" Febuary.
Laboratory monthly progress report for the Saturn 1B program between dates Febuary 1st through Febuary 31st, 1967. -
"Test Laboratory monthly progress report" April.
Laboratory monthly progress report for the Saturn 1B program between dates April 1st through April 31st, 1967. Last page of document is missing. -
"Test Laboratory monthly progress report" June.
Laboratory monthly progress report for the Saturn 1B program between dates June 1st through June 31st, 1967. -
"Test Laboratory monthly progress report" September.
Laboratory monthly progress report for the Saturn 1B program between dates September 1st through September 31st, 1967. -
"Test Laboratory monthly progress report" January.
Laboratory monthly progress report for the Saturn 1B program between dates January 1st through January 31st, 1968. -
"Apollo Vehicle Propulsion Systems."
This paper discusses the propulsion requirements for various stages of the Apollo vehicles and the development of these engines. -
Memorandum to update the "Apollo/Saturn Logistics Support Requirements Plan."
This memorandum contains the pages to be changed in the logistics program for the Apollo/Saturn Project. The logistics plan includes the design, procuring, manufacturing, and production processes. This plan formalizes the program, improves logistic support, and implements management and action plans. -
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. -
"Space Division, North American Rockwell Corporation Organizational Chart."
Organization chart for North American Rockwell, 1968 -
Space age vision [photograph].
8 x 10 inch black and white photograph. -
"Welcome back planned for 'Gum drop' crew."
News article detailing the planned 'Welcome back' events surrounding the resturn of the Apollo 9 crew. -
"Craft destined for use in lunar landing mission."
News article detailing how the Apollo spacecraft 107 command modules are planned to be used in future space-missions. -
"SII, with all spray foam insulation MTF-bound."
News article detialing the innovation of the SII's design, specifically how it is made lighter. -
"New Liftoff date only change in Apollo 10 mission."
News article detailing the slight change in schedule regarding the Apollo 10 lunar module's take-off from the Moon and its return to Earth. -
"Apollo 9 command module arrives home."
News article detialing the recovery of the Apollo 9 command module and the events planned around its display. -
"Apollo 9 flight ends; Astronauts return."
News article detailing the recovery of the Apollo 9 crew after their mission -
"July 16th still set as Apollo 11's 'L-Day.'"
News article confirming NASA's announcement of Apollo 11's launch-day. Focuses on the optimism surrounding the launch as well. -
"July 16th confirmed as definite for Apollo 11."
News article covering NASA's announcement of Apollo 11's launch-date: July 16th. -
"Five manned Apollo flights scheduled this year."
News article detailing the planning of five more projects after the successful mission of Apollo 8. -
"Astronaut trio sees 'successful' Apollo 9 mission."
News article detailing the hope from the Apollo 9 crew that their mission will be a success. -
"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. -
"Apollo countdown begins on Monday."
News article detailing the interest around the liftoff of the Apollo 8 spacecraft. -
"S-IC stage, S-II stage, S-IVB stage, instrument unit drawing."
8 x 10 inch black and white photograph.; Image includes dimensions and labels of exterior features of the rocket. -
"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. -
"S-IC heat shield illustration."
The drawing gives information about the honeycomb and edge rolled construction of a heat-shield plate. -
"Stabilized mechanical properties [table] photograph.
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. -
"Alloy designation" Table.
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. -
"M-45 casting alloy : Gyro stabilizer support."
8 x 10 inch black and white photograph of a gyro stabilizing support. -
"Table V : mechanical properties of aluminum casting alloys."
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. -
"Table IV : chemical composition of M-45 and other high strength aluminum casting alloys."
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. -
"Table II : comparison of typical mechanical properties of experimental alloys with commercial alloys."
8 x 10 inch black and white photograph of a table comparing the tensile strength of each alloy in relation to a desired goal. -
"Table I : chemical composition of experimental alloys."
8 x 10 inch black and white photograph of a table reperesenting the chemical composition of alloys M825 and M826.