• DocumentCode
    888733
  • Title

    The effects of 1 kW class arcjet thruster plumes on spacecraft charging and spacecraft thermal control materials

  • Author

    Bogorad, A. ; Lichtin, D.A. ; Bowman, C. ; Armenti, J. ; Pencil, E. ; Sarmiento, C.

  • Author_Institution
    General Electric Co., Princeton, NJ, USA
  • Volume
    39
  • Issue
    6
  • fYear
    1992
  • fDate
    12/1/1992 12:00:00 AM
  • Firstpage
    1783
  • Lastpage
    1789
  • Abstract
    Arcjet thrusters are soon to be used for north/south stationkeeping on commercial communications satellites. A series of tests was performed to evaluate the possible effects of these thrusters on spacecraft charging and the degradation of thermal control material. During the tests the interaction between arcjet plumes and both charged and uncharged surfaces did not cause any significant material degradation. In addition, firing an arcjet thruster benignly reduced the potential of charged surfaces to near zero
  • Keywords
    aerospace propulsion; electric propulsion; spacecraft charging; thermal insulation; 1 kW; arcjet thruster plumes; commercial communications satellites; north/south stationkeeping; spacecraft charging; thermal control materials; Aircraft manufacture; Electrostatic discharge; Electrostatic interference; Firing; Propulsion; Space vehicles; Surface charging; Surface contamination; Surface discharges; Thermal pollution;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/23.211367
  • Filename
    211367