• DocumentCode
    2465895
  • Title

    Discharge over spacecraft insulator surface in low Earth orbit plasma environment

  • Author

    Cho, Mengu ; Miyata, Naoki ; Hikita, Masayuki ; Sasaki, Susumu

  • Author_Institution
    Kyushu Inst. of Technol., Kitakyushu, Japan
  • Volume
    2
  • fYear
    1998
  • fDate
    17-21 Aug 1998
  • Firstpage
    804
  • Abstract
    When a spacecraft operates at a high voltage, the spacecraft body potential become highly negative with respect to the surrounding plasma. A laboratory experiment has been carried out to study the interaction between the spacecraft insulator surface and the plasma. Once a discharge occurs through the insulator at one point on the surface, the positive current to the circuit drives the conductor potential, which lies below the insulator, positive. The potential of the un-discharged surface increases as the conductor potential increases and collects electrons by neutralizing all the positive charge stored before the discharge. The current path of RC discharge is formed between the discharge spot and the un-discharged insulator surface, which acts as the capacitance, through the plasma resistance and the spacecraft circuit resistance. An ion acoustic wave was detected by a Langmuir probe, which was launched by the potential jump of the un-discharged surface. There is a possibility that a very large amount of current flows into the spacecraft body circuit because the capacitance of the entire spacecraft surface is very large
  • Keywords
    aerospace simulation; aerospace testing; electric charge; insulators; plasma; space vehicles; spacecraft charging; surface charging; surface discharges; Langmuir probe; RC discharge current path; capacitance; ion acoustic wave; laboratory experiment; low Earth orbit plasma environment; negative body potential; plasma resistance; positive conductor potential; positive current; spacecraft circuit resistance; spacecraft insulator surface discharge; un-discharged surface potential; Capacitance; Circuits; Conductors; Insulation; Low earth orbit satellites; Plasmas; Space vehicles; Surface acoustic waves; Surface discharges; Surface resistance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Discharges and Electrical Insulation in Vacuum, 1998. Proceedings ISDEIV. XVIIIth International Symposium on
  • Conference_Location
    Eindhoven
  • ISSN
    1093-2941
  • Print_ISBN
    0-7803-3953-3
  • Type

    conf

  • DOI
    10.1109/DEIV.1998.738895
  • Filename
    738895