• DocumentCode
    1856608
  • Title

    Space-hardware design for long life with high reliability

  • Author

    Gindorf, Tom E. ; Miles, Ralph F. ; Murphy, Gerald B.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    1994
  • fDate
    24-27Jan 1994
  • Firstpage
    338
  • Lastpage
    341
  • Abstract
    In 1991, the Cassini Project, NASA´s planetary project to place a spacecraft in orbit about Saturn, funded a study at the Jet Propulsion Laboratory (JPL) to identify rules for design and test of hardware required to function reliably in space for very long lifetimes. Twenty-nine subjects were considered comprising 130 specific rules related to long-life issues such as accelerated life testing, cycling of mechanical devices, selection and application of parts, semiconductor junction temperatures, and worst-case analysis for long life. The study was subsequently published as a JPL document. One major conclusion of the workshop was that unattended space missions extending out to 25 years or more are feasible. The paper reports on the study and the one-day workshop
  • Keywords
    life testing; reliability; software reliability; Cassini Project; Jet Propulsion Laboratory; NASA´s planetary project; Saturn; accelerated life testing; cycling; high reliability; long life; mechanical devices; semiconductor junction temperatures; space-hardware design; worst-case analysis; Hardware; Laboratories; Life estimation; Life testing; Planetary orbits; Propulsion; Saturn; Space missions; Space vehicles; Temperature;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1994. Proceedings., Annual
  • Conference_Location
    Anaheim, CA
  • Print_ISBN
    0-7803-1786-6
  • Type

    conf

  • DOI
    10.1109/RAMS.1994.291131
  • Filename
    291131