• DocumentCode
    1329263
  • Title

    Maintainability Design Requirements for Future Space Systems

  • Author

    Peterson, Elmer L.

  • Author_Institution
    Space and Information Systems Division, North American Aviation, Inc., Downey, Calif.
  • Issue
    1
  • fYear
    1966
  • fDate
    5/1/1966 12:00:00 AM
  • Firstpage
    17
  • Lastpage
    21
  • Abstract
    Design requirements which consider maintenance capability can be expected to be quite different for space system application when compared to those currently in use for today´s weapon systems. Needs will vary, as will the base for the definition of quantized criteria. Maximum urgency is placed on crew safety, mission success, and meeting a launch window. The expressions for quantitative maintainability design criteria will shift from the familiar ``Meantime´´ base to one of ``Allowable Time,´´ ``Probability of Repair Within Time Limits,´´ and ``Expenditure of Human Energy.´´ This paper explores the operational requirements for maintainability in future space systems, discusses interface problems, and defines quantized maintainability objectives for the different applications of 1) spacecraft, 2) space stations, 3) boosters, and 4) support equipment.
  • Keywords
    Current measurement; Extraterrestrial measurements; Fault diagnosis; Humans; Maintenance; Safety; Space missions; Space stations; Space vehicles; Weapons;
  • fLanguage
    English
  • Journal_Title
    Reliability, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9529
  • Type

    jour

  • DOI
    10.1109/TR.1966.5217585
  • Filename
    5217585