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Effect of Anode Dielectric Coating on Hall Thruster Operation.


DE2004820110

Publication Date 2003
Personal Author Dorft, L.; Raitses, Y.; Fisch, N. J.; Semenov, V.
Page Count 20
Abstract An interesting phenomenon observed in the near-anode region of a Hall thruster is that the anode fall changes from positive to negative upon removal of the dielectric coating, which is produced on the anode surface during the normal course of Hall thruster operation. The anode fall might affect the thruster lifetime and acceleration efficiency. The effect of the anode coating on the anode fall is studied experimentally using both biased and emissive probes. Measurements of discharge current oscillations indicate that thruster operation is more stable with the coated anode.
Keywords
  • Hall thruster
  • Anodes
  • Dialectics
  • Anodic coatings
  • Protective treatment
  • Thrusters
  • Coatings
  • Probes
  • Measurements
  • Stability
  • Oscillations
  • Dialectic coating
  • Biased probes
  • Emissive probes
Source Agency
  • Technical Information Center Oak Ridge Tennessee
Corporate Authors Princeton Univ., NJ. Plasma Physics Lab.; Department of Energy, Washington, DC.
Supplemental Notes Sponsored by Department of Energy, Washington, DC.
Document Type Technical Report
NTIS Issue Number 200414
Effect of Anode Dielectric Coating on Hall Thruster Operation.
Effect of Anode Dielectric Coating on Hall Thruster Operation.
DE2004820110

  • Hall thruster
  • Anodes
  • Dialectics
  • Anodic coatings
  • Protective treatment
  • Thrusters
  • Coatings
  • Probes
  • Measurements
  • Stability
  • Oscillations
  • Dialectic coating
  • Biased probes
  • Emissive probes
  • Technical Information Center Oak Ridge Tennessee
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