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"Evolutionary Steps in S-IVB Development."
The injection stage of a multistage launch vehicle must be partially a velocity stage and partially a spacecraft; it must not only boost the payload, it must also perform cooperative mission operations with the payload after orbital insertion. These hybrid requirements result in intrinsic stage versatility which permits consideration of new and challenging missions for the stage which were unanticipated during initial design.; Prepared by T. J. Gordon, Director, Advance Space Stations and Planetary Systems, Space Systems Center, Douglas Aircraft Company, Huntington Beach, California. -
"Evolution of a Space Capability."
Two different organizational charts. -
"Extensions of Saturn."
This paper discusses the possible applications of Saturn vehicles to future space exploration. Potential missions utilizing Apollo derived hardware are examined. Research, development, and operations in earth orbit as well as lunar exploration, unmanned and manned interplanetary exploration are reviewed. These hypothetical missions are discussed in the context of the present and potential capability of three configurations of the Saturn vehicle; an uprated Saturn I, a three-stage Saturn V and a four-stage Saturn V. NOTE: Work presented herein was conducted by the Douglas Missiles and Space Systems Division under company-sponsored research and development funds. Therefore, the concepts and objectives described within this paper reflect the opinions of the authors and do not necessarily constitute endorsement by NASA, the Air Force, or any other U.S. Government organization. The nominal performance numbers presented are typical of the current configurations and possible future vehicle configurations. -
"Fabrication of Plenum Tanks by Explosive Forming and Electron Beam Welding."
This report presents the results of a program initiated to study the use of explosive forming and electron beam fusion welding techniques in the fabrication of pressurized cryogenic materials containers. Using these techniques, vessels were successfully formed from 304 stainless steel and X7106 aluminum alloy in the T63 condition.; Manufacturing Research and Technology Division.; Manufacturing Engineering Laboratory.; Research and Development Operations. -
"Fabricating the Saturn S-IC Booster."
AIAA Second Annual Meeting, San Francisco, California. Discusses the fabrication process of the Saturn S-IC booster. -
"Facility Design for Handling Liquid Hydrogen for Space Vehicle Applications."
Presented to German Society for Rocket Technology & Astronautics.Essay discussing the capabilities of liquid hydrogen as fuel. -
"Facilities Engineering for the National Aeronautics and Space Administration."
Article makes references to a film. Centers around the idea that testing space vehicles extensively before launch is cost control. -
"Fact Sheet : IBM Computer Will Direct Saturn Orbital Test Flight."
Press release regarding a IBM digital computer directing a Saturn 1B orbital mission. -
"Failure Investigations of Large Liquid Propelled Rocket Engine Components."
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. -
"Films List : NASA Motion Picture Film Service Area Five: Alabama - Kentucky - Louisiana - Mississippi - Tennessee."
A list of films oriented towards the National Space Program and other related topics.