UAH Archives, Special Collections, and Digital Initiatives

Browse Items (47 total)

  • omsfprogstatrevimannspacfligschevoluIIIlaunvehibookengieditA_081007091345.pdf

    OMSF Program Status Review October 1965.; Edition "A"
  • mateinspacexpl_080107092258.pdf

    This paper presents a general review of major structural alloys that have been used in liquid rockets and space vehicles, the current state-of-the-art as applied to the Apollo launch vehicle systems, and discusses some materials currently under development for future requirements in vehicles for space exploration. Some aspects of the importance of corrosion resistant materials and suitable protective measures are discussed, as applied to both flight hardware and associated ground support equipment.
  • nextstopthemoon_030209161111.pdf

    Release describing the launch of the Apollo 11.
  • PRATTW~1.PDF

    Photograph of a Pratt & Whitney rocket engine.
  • proincrypumdesforspaapp_031808115456.pdf

    Report detailing the problems surrounding cryogenic pump design for space travel and missions.
  • Proplect_091907133304.pdf

    Lecture discussing the types of propellant used in space rockets.
  • recenasaexphydeng_070307131651.pdf

    This paper presents a review of the experience which has accumulated in the development of the Liquid Hydrogen J-2 and RL10 rocket engines. These engines are being developed by the Rocketdyne Division of North American Aviation and Pratt & Whitney Aircraft, a Division of United Aircraft Corporation respectively.; On NASA Technical Reports Server (NTRS) as Unclassified; No Copyright; Unlimited; Publicly available. Also found on AIAA site.
  • recnasexpwithydeng_041207110126.pdf

    This paper presents a review of the experience which has accumulated in the development of the Liquid Hydrogen J-2 and RL10 rocket engines. These engines are being developed by the Rocketdyne Division of North American Aviation and Pratt & Whitney Aircraft, a Division of United Aircraft Corporation respectively.; On NASA Technical Reports Server (NTRS) as Unclassified; No Copyright; Unlimited; Publicly available. Also found on AIAA site.
  • Reliqualmana_080707155107.pdf

    The role of Reliability and Quality in NASA program management is well defined by the NPC 200 series and complimentary procurement regulations.
  • 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.
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