UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8239 total)

  • Defense_Billboard_138_001.pdf
  • spc_lude_008_026.pdf

    The pamphlet includes a reprint of an article from RCAA publication Space Journal, a history of the organization with photos, and membership information.
  • Rockengiselecrit_042908141859.pdf

    This paper considers many of the factors and criteria which have to be considered and evaluated when selecting a specific rocket engine for a given vehicle application. The lists of criteria can be helpful as checklists in design and systems engineering of a rocket propulsion device. About ten different applications are examined to illustrate the relative importance of some of these selection criteria. There will be groupings of our major types of criteria; namely, performance, operational, economic and so-called judgment criteria. In many cases the last three categories are equally or more important than the performance criteria in selecting one of several rocket engines for a specific application. The actual selection usually is a compromise to make the rocket engine responsive to several important criteria.
  • Rockengiturbspactrav_101507142613.pdf

    Finding the turbopump arrangement which is best suited for a given rocket engine - space travel applications - constitutes an important task. The arrangement depends upon a large variety of different factors, such as, the engine cycle, weight, the liquids to be pumped, the cavitation performance, the bearings and their lubrication, the seals and the turbine. In this report these factors and their influence on the turbopump configuration are discussed. It is shown that three of them: weight, propellants to be pumped and obtainable suction performance have the largest influence on the selection of the turbopump. A systematic approach is outlines for the design process, which allows to arrive at a turbopump arrangement best suited for a given application.
  • rockexheffects_071707095315.pdf

    Presented by Olen P. Ely, National Aeronautics and Space Administration, Marshall Space Flight Center, Huntsville, Alabama and R. W. Hockenberger, International Business Machines. Paper that explores the effects of rocket-engine exhaust on radio-signals.
  • scan0011rev_080107115810.jpg

    8 x 10 inch black and white photograph of a rocket motor material list. The weight of the material is measured in pounds.
  • spc_dann_000168.mp4

    Roofing work continues on the Dannenbergs' new house. In this film, the roof is being built over the family room. Klaus Dannenberg is shown climbing up onto the roof to check it out. Summer/Autumn 1958.
  • spc_dann_000167.mp4

    This film focuses on the roofing work on the Dannenbergs' new house. Shown are workers trimming the eaves of the roof as well as nailing down the weatherproof cover to the top of the roof. Summer/Autumn 1958.
  • spc_nick_000450_000457.pdf

    Various handwritten notes on the Army missile program and other information pertaining to the case of Colonel John C. Nickerson, Jr.
  • scan0020rev_080107140240.jpg

    The drawing gives information about the honeycomb and edge rolled construction of a heat-shield plate.