• DocumentCode
    827314
  • Title

    Low Power CAMAC and NIM Modular Systems for Spaceflight Use on Shuttle and Spacelab Missions

  • Author

    Trainor, James H. ; Kaminski, Thomas J. ; Ehrmann, Charles H.

  • Author_Institution
    NASA/Goddard Space Flight Center Greenbelt, Maryland 20771
  • Volume
    24
  • Issue
    1
  • fYear
    1977
  • Firstpage
    835
  • Lastpage
    839
  • Abstract
    The advent of the Shuttle launch vehicle and Spacelab have resulted in adequate weight and volume such that experiment electronics can be implemented at relatively low cost using spaceflight versions of CAMAC and NIM modules. Studies of 10 modules by manufacturers have shown that power reduction overall by a factor of ~ 3 can be accomplished. This is adequate both from the point of view of consumption and temperature rise in vacuum. Our studies have shown that a stock of ~ 45 module types is required and a listing is given. The changes required in these modules in order to produce spaceflight versions are described. And finally, the further studies, prototyping and testing leading to eventual flight qualification are described.
  • Keywords
    Acoustical engineering; Aerospace engineering; CAMAC; NASA; Payloads; Satellites; Space missions; Space shuttles; Space vehicles; Testing;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/TNS.1977.4328790
  • Filename
    4328790