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Investigation of the start transient in a Hall thruster

  • H. Liu*
  • , D. R. Yu
  • , G. J. Yan
  • , J. Y. Liu
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

A two dimensional axisymmetric fully kinetic Particle-in-Cell/Monte Carlo Collision (PIC-MCC) model is used to describe the ignition process in a Hall thruster. A current peak and latter the periodic oscillation of current and electric potential are found. The corresponding evolutions of plasma density, electric potential and atom density during the ignition process are introduced in the paper. In addition, influences of mass flow rate and discharge potential on current peak are modeled and analyzed. The simulated results are consistent with former experimental results.

Original languageEnglish
Pages (from-to)603-611
Number of pages9
JournalContributions to Plasma Physics
Volume48
Issue number9-10
DOIs
StatePublished - Dec 2008

Keywords

  • Hall thruster
  • Ignition
  • Particle-in-cell
  • Simulation

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