• DocumentCode
    969363
  • Title

    Laboratory Experiments for Code Validation of Multiutility Spacecraft Charging Analysis Tool (MUSCAT)

  • Author

    Hosoda, Satoshi ; Muranaka, Takanobu ; Kuninaka, Hitoshi ; Kim, Jeongho ; Hatta, Shinji ; Kurahara, Naomi ; Cho, Mengu ; Ueda, Hiroko O. ; Koga, Kiyokazu ; Goka, Tateo

  • Author_Institution
    Inst. of Space & Astronaut. Sci., Japan Aerosp. Exploration Agency, Sagamihara
  • Volume
    36
  • Issue
    5
  • fYear
    2008
  • Firstpage
    2350
  • Lastpage
    2359
  • Abstract
    The multiutility spacecraft charging analysis tool (MUSCAT), a spacecraft charging analysis software, has been developed as a collaboration work between Japan Aerospace Exploration Agency and Kyushu Institute of Technology. Laboratory experiments for fundamental code validation were carried out in both facilities´ plasma chambers. MUSCAT is a particle simulation code based on particle-in-cell (PIC) and particle tracking (PT) algorithms capable of calculating the floating-body potential of a spacecraft with respect to the plasma potential. Three experiments were carried out regarding spacecraft-plasma interaction phenomena important in LEO and PEO. A Langmuir probe was used to measure the current collection and potential distribution in static plasma to validate the PIC and PT schemes. The floating potential of an object in plasma with an energetic electron component was measured to validate the floating-body calculation as well as the PT scheme. Current collection and potential distribution in the wake structure were measured to validate the PIC and PT scheme in flowing plasma condition. The experimental results and the simulation results agreed very well in all the three experiments, validating the accuracy of the MUSCAT solver.
  • Keywords
    aerospace computing; plasma; space vehicles; LEO; Langmuir probe; PEO; code validation; laboratory experiments; multiutility spacecraft charging analysis tool; particle simulation code; particle tracking algorithm; particle-in-cell algorithm; spacecraft charging analysis software; spacecraft-plasma interaction phenomena; Simulation software; spacecraft charging; wake plasma;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/TPS.2008.2003973
  • Filename
    4663156