• DocumentCode
    1180240
  • Title

    Line Replaceable Unit (LRU) Analysis in the Space Shuttle Orbiter Electrical Power System

  • Author

    Oepomo, Tedja Santanoe

  • Author_Institution
    Space Transportation and Systems Group Rockwell International
  • Issue
    12
  • fYear
    1985
  • Firstpage
    3501
  • Lastpage
    3509
  • Abstract
    The National Aeronautics and Space Administration (NASA) Space Shuttle orbiter, as a test bed for low-orbit space laboratory experiments, needs an orbiter voltage analysis on all orbiter line replaceable units (LRU´s). This analysis should use a mathematical model to predict voltages at the various LRU´s so that voltage drops from a bus to an LRU can then be computed based on calculated resistance of the conductors and load current.
  • Keywords
    Conductors; Laboratories; Mathematical model; NASA; Orbital calculations; Power system analysis computing; Power system modeling; Space shuttles; Testing; Voltage;
  • fLanguage
    English
  • Journal_Title
    Power Apparatus and Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9510
  • Type

    jour

  • DOI
    10.1109/TPAS.1985.318902
  • Filename
    4113049