UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8239 total)

  • TVsystapoltele_111307142704.pdf

    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.
  • Sperrandmontprog_092910151001.pdf

    The following pages contain reports for each of the individual contract appendices covering technical progress and accomplishments, related problems, and staffing progress. The report of manhours expended against each appendix by schedule order is being submitted as a part of the financial management report.
  • earorbworkcapbrochA_021110095433.pdf.pdf

    A brochure designed to depict a competence and capability in the area of large earth-orbital workshops.
  • enggcappresentation.pdf.pdf

    This Engineering Capabilities Presentation lists the competence and capability that has been demonstrated by the Space Support Division of Sperry Rand Corporation while fulfilling contractual commitments in the aerospace industry. This is a preliminary presentation; the preparation of a complete capabilities history of the division is currently in the developmental stage. The Capabilities Experience Summary is comprised of ten categories. e.g. Category 1 - Aeronautics, etc. The capabilities reported herein were performed by the Space Support Division under Contract NAS8-20055 to the National Aeronautics and Space Administration, George C. Marshall Flight Center, Astrionics Laboratory, Huntsville, Alabama.
  • sdsp_skyl_000070_001.pdf
  • satIfliteseval_070507143020.pdf

    As this paper is being written, the Saturn I flight test program includes five flights launched between October, 1961 and January, 1964. All five fiights were complete successes, both in achieving all major test missions and in obtaining an unprecedented volume of system performance data for flight analysis.
  • http://dkdayton.net/roberts/images/r04a/pdfs/r04a14-19.pdf
  • spc_nick_000314_000314.pdf

    Sparkman thanks Nickerson for sending a booklet he had requested. He also requests Nickerson to send information on a long range flight conducted by ABMA directly to Erik Bergaust for an interview Bergaust did on Sparkman.
  • spc_stnv_000065.pdf
  • SaturnIBSA217_052008142122.pdf

    This document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical-mile circular orbit is 44,965 pounds. The Saturn IB SA-217 launch vehicle is to be used as the baseline vehicle for advanced studies requiring the use of the standard or modified Saturn IB launch vehicle. This vehicle definition does not necessarily represent approved changes to any specific vehicle. This document supersedes the Saturn IB SA-213 reference Launch Vehicle, described in memorandum R-P&VE-DIR-65-92.