UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8218 total)

  • http://dkdayton.net/roberts/images/r04c/pdfs/r04c04-06.pdf
  • http://dkdayton.net/roberts/images/r04c/pdfs/r04c04-05.pdf
  • rptno24fragge_082707112230.pdf

    Memo to Lee Cropp, I-RM-D concerning security classification.
  • cleandconcon_071107110215.pdf

    The document is a paper describing contamination cleaning methods and advocating for further developments in the field. Tables and figures are included at the end of the paper. The figures include a comparison of Saturn V with Saturn I and Saturn IB and cross-sections of the Saturn C-5, S-IC stage fuel tank assembly and oxidizer tank assembly.
  • Nortamerrockjul1169_010711121426.pdf

    A news article detailing the scheduled launch for the Apollo 11. "Eagle" is the name of the lunar module and "Columbia" is the name of the service module.
  • commprobrelaluna_022807133241.pdf

    "This technical note concerns some of the problems encountered with the landing of a payload on the moon. The main problem areas such as guidance, velocity control and impact considerations are discussed. Although no final conclusions or designs are intended, it is hoped that the material presented will serve as a guide for future detailed work."
  • commbulkdraw.jpg.jpg

    8 x 10 inch black and white photograph; This is a cutaway drawing of the bulkhead with information about the LH2 tank skin, insulation, Aft LOX bulkhead, 2014-T6 alum skin and fiberglass core. Part of an envelope with photos accompanying C. E. Cataldo paper "Materials in Space Exploration."
  • freedomadober2_022607111422.pdf

    Includes bibliographical references.; Original format: paperback book (42 pages); Cover title: Resources for freedom : the outlook of energy resources, volume III. Contains plans and analyses of potential future energy sources.
  • comsysbladurreeoflarveh_031808114618.pdf

    This paper was published in the Proceedings of the IEEE, volume 55, number 5, May 1967.; ABSTRACT: Much of the theoretical research on reentry blackout is in a format difficult for the communications design engineer to use in his system analysis. This paper derives simplified equations for the average sheath power loss that may be added (in dB) to the usual space loss to obtain an approximate total propagation loss. The plasma and sheath properties are discussed in detail but largely without supporting mathematics, in order to give the design engineer a better understanding of the overall problem. For the same reason and to provide insight into the final results, the average radiated power is found, using both intuitive and rigorous techniques. Several graphs of plasma properties are included in the development as an aid to numerical computation, and results are compared with the work of other authors.
  • SkywSpacDiviVolXXIX17_052410122936.pdf

    A news article detailing the winners of scholarships from a competition held by Space Division. This contest was held for the children of Space Division employees.