• DocumentCode
    797658
  • Title

    The Evolution of IMP Spacecraft Mosfet Data Systems

  • Author

    White, Hosea D., Jr. ; Lokerson, Donald C.

  • Author_Institution
    Data Techniques Branch, Electronics Division Goddard Space Flight Center, NASA Greenbelt, Maryland 20771
  • Volume
    18
  • Issue
    1
  • fYear
    1971
  • Firstpage
    233
  • Lastpage
    236
  • Abstract
    Since 1964 the Interplanetary Monitoring Platform spacecraft data systems have used MOSFET devices. Many millions of device hours have been accumulated from IMPs D,E,F and G in orbit without any "proven failures" (two possible non-catastrophic failures may have occurred on MOSFET chips in IMP-D well after a year in orbit). We are now using the fourth generation of MOSFET blocks in IMPs H&J where there are approximately 1000 devices on a single chip. Historically, the development of MOSFET blocks for the IMP program has progressed through four phases. The PHASE I blocks contained about 10 devices/chip, PHASE II about 50, PHASE III about 200 and presently the PHASE IV blocks contain about 1000 devices/chip. The PHASE IV data system now under fabrication uses approximately one-half million devices. This two orders of magnitude increase in the number of devices per chip, while vastly increasing the capability of the data system, has also revised the thinking used in system design and has revised the reliability approach used.
  • Keywords
    Ambient intelligence; Analog-digital conversion; Control systems; Data systems; Logic devices; MOSFET circuits; Manufacturing processes; Production; Resistors; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/TNS.1971.4325871
  • Filename
    4325871