• DocumentCode
    3237377
  • Title

    Designing electronic systems for space

  • Author

    Sunderland, David A. ; Lerma, Jaime ; McKay, Anthony L.

  • Author_Institution
    Boeing Space & Intell. Syst., El Segundo, CA
  • fYear
    2008
  • fDate
    13-15 Oct. 2008
  • Firstpage
    171
  • Lastpage
    177
  • Abstract
    This tutorial presents the unique issues that must be considered when designing electronics for space applications (including, but not limited to, radiation effects), and how key satellite system building blocks are affected by these issues. We review the common design techniques used to mitigate these effects, with an emphasis on those used within custom bipolar integrated circuits. Finally, we discuss the requirements for characterization and qualification of the resulting products.
  • Keywords
    bipolar integrated circuits; space vehicle electronics; custom bipolar integrated circuits; electronic systems; satellite system; space applications; space vehicle electronics; spacecraft; Aerospace electronics; Artificial satellites; Bipolar integrated circuits; Ionizing radiation; Job shop scheduling; Land surface temperature; Radiation effects; Single event upset; Solar heating; Space vehicles; bipolar integrated circuits; radiation effects; radiation hardening; reliability; space vehicle electronics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Bipolar/BiCMOS Circuits and Technology Meeting, 2008. BCTM 2008. IEEE
  • Conference_Location
    Monteray, CA
  • ISSN
    1088-9299
  • Print_ISBN
    978-1-4244-2725-3
  • Electronic_ISBN
    1088-9299
  • Type

    conf

  • DOI
    10.1109/BIPOL.2008.4662737
  • Filename
    4662737