• DocumentCode
    976281
  • Title

    Spacecraft charging potential during electron-beam injections into space plasmas

  • Author

    Lin, Chin S. ; Koga, James

  • Author_Institution
    Dept. of Space Sci., Southwest Res. Inst., San Antonio, TX, USA
  • Volume
    17
  • Issue
    2
  • fYear
    1989
  • fDate
    4/1/1989 12:00:00 AM
  • Firstpage
    205
  • Lastpage
    209
  • Abstract
    Injections of nonrelativistic electron beams from an infinite conductor have been simulated by using a two-dimensional electrostatic particle code to study the spacecraft charging potential. The simulations show that the conductor charging potential at the end of simulations does not vary with the beam density when the beam density exceeds four times the ambient density. The reflection coefficient, which determines a percentage of incident electrons reflected by the conductor, increases the charging potential. To charge the conductor to the beam energy, the reflection coefficient needs to be about 0.5. The results are applied to explain the spacecraft charging potential measured during the SEPAC (Space Experiments with Particle Accelerators) experiments from Spacelab 1
  • Keywords
    electric potential; electron beam effects; ionosphere; plasma; plasma density; plasma-beam interactions; space vehicles; SEPAC; Space Experiments with Particle Accelerators; Spacelab 1; atmosphere; charging potential; conductor; density; electron-beam injections; ionosphere; nonrelativistic electron beams; reflection coefficient; space plasmas; space vehicles; spacecraft; two-dimensional electrostatic particle code; Conductors; Electron beams; Ionosphere; Optical reflection; Particle beams; Plasma accelerators; Plasma measurements; Plasma simulation; Space shuttles; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/27.24626
  • Filename
    24626