UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8239 total)

  • evoofaspacap_031507074311.pdf

    Two different organizational charts.
  • evolairc_071207092817.pdf

    Illustration depicting the history of airplanes across a graph.
  • http://dkdayton.net/roberts/images/r04c/pdfs/r04c04-23.pdf
  • evoofthesatboo.jpg

    8 x 10 inch Black & White photograph. MS-G 103-63 Nov. 22, 63 is on the photograph. Displays the evolution of space-rocket designs side-by-side.
  • EvolstepsinS-IVBdevelopment_061708170306.pdf

    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.
  • Defense_Billboard_71_001.pdf
  • Defense_Billboard_73_001.pdf
  • Extesatu_111307104548.pdf

    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.
  • Fabrsatus-icboos_081407122702.pdf

    AIAA Second Annual Meeting, San Francisco, California. Discusses the fabrication process of the Saturn S-IC booster.
  • Fabrofplentankbyexplformandelecbeamweld_111507104932.pdf

    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.