• DocumentCode
    1411557
  • Title

    Some Novel Ideas of Spacecraft Charging Mitigation

  • Author

    Lai, Shu T.

  • Author_Institution
    Dept. of Aeronaut. & Astronaut., Massachusetts Inst. of Technol., Cambridge, MA, USA
  • Volume
    40
  • Issue
    2
  • fYear
    2012
  • Firstpage
    402
  • Lastpage
    409
  • Abstract
    The level of spacecraft surface charging is determined by current balance. At geosynchronous altitude, photoelectron currents from spacecraft surfaces exceed the ambient electron currents. Lacking photoemission, however, the dark side of a spacecraft can charge to high negative voltages, which, in turn, affect the sunlit side. This paper explores the feasibility of using the following: 1) mirrors and 2) artificial photon sources, such as xenon excimer lamps or vacuum ultraviolet LEDs, to generate sufficient photoemission from the dark side to prevent high-level negative voltage charging.
  • Keywords
    photoemission; space vehicles; surface charging; ambient electron currents; artificial photon sources; geosynchronous altitude; high-level negative voltage charging; mirrors; photoelectron currents; photoemission; spacecraft charging mitigation; spacecraft surface charging; spacecraft surfaces; vacuum ultraviolet LED; xenon excimer lamps; Dielectrics; Electric potential; Materials; Mirrors; Photoelectricity; Space vehicles; Surface charging; Mitigation; photoelectrons; space plasmas; spacecraft charging;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/TPS.2011.2176755
  • Filename
    6118330