• DocumentCode
    3379454
  • Title

    Space radiation effects and reliability considerations for the proposed Jupiter Europa Orbiter

  • Author

    Johnston, Allan

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2011
  • fDate
    10-14 April 2011
  • Abstract
    The proposed Jupiter Europa Orbiter (JEO) mission to explore the Jovian moon Europa poses a number of challenges. The spacecraft must operate for about seven years during the transit time to the vicinity of Jupiter, and then endure unusually high radiation levels during exploration and orbiting phases. The ability to withstand usually high total dose levels is critical for the mission, along with meeting the high reliability standards for flagship NASA missions. Reliability of new microelectronic components must be sufficiently understood to meet overall mission requirements.
  • Keywords
    Jupiter; geophysical prospecting; integrated circuits; radiation effects; reliability; space vehicle electronics; space vehicles; Jovian moon Europa; Jupiter Europa Orbiter; NASA mission; microelectronic component; reliability; space radiation effect; transit time; Integrated circuit reliability; Space missions; Temperature distribution; Testing; Transistors; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability Physics Symposium (IRPS), 2011 IEEE International
  • Conference_Location
    Monterey, CA
  • ISSN
    1541-7026
  • Print_ISBN
    978-1-4244-9113-1
  • Electronic_ISBN
    1541-7026
  • Type

    conf

  • DOI
    10.1109/IRPS.2011.5784471
  • Filename
    5784471