• DocumentCode
    482442
  • Title

    An experimental study of local magnetic field intensity effects on the discharge characterization of Hall thrusters

  • Author

    Peng, E. ; Yu, Daren ; Han, Ke ; Shang, Fang ; Chen, Chao ; Zhao, Xin-shuang ; Zhan, Yan

  • Author_Institution
    Harbin Inst. of Technol., Harbin
  • fYear
    2008
  • fDate
    17-20 Oct. 2008
  • Firstpage
    920
  • Lastpage
    925
  • Abstract
    This paper investigates the magnetic field intensity effects on the discharge characterization of Hall thrusters for optimization of the magnetic fields. Vary the strength of magnetic fields with its topography holds constant (keep in ldquofocusingrdquo type), and make an experimental study of the thrusterpsilas operating performance working in different regions of magneto-ampere curve through Langmuir probe, spectrograph, etc. Detailed examination of the results shows that when the magnitude of magnetic field intensity less than its critical value, near-wall conductivity give priority to the activity that electrons traverse the magnetic field, if not, discharge current varying with magnetic field intensity abnormally, and existing electrons conductive theories are failed to explain this phenomenon.
  • Keywords
    aerospace propulsion; magnetic field effects; plasma accelerators; Hall thrusters; discharge characterization; local magnetic field intensity effects; Acceleration; Chaos; Conductivity; Electrons; Ionization; Magnetic fields; Plasma accelerators; Plasma sheaths; Probes; Surfaces;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical Machines and Systems, 2008. ICEMS 2008. International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-3826-6
  • Electronic_ISBN
    978-7-5062-9221-4
  • Type

    conf

  • Filename
    4770846