Simulation of double stage hall thruster with double-peaked magnetic field

  • Yongjie Ding
  • Peng Li
  • Hezhi Sun
  • Liqiu Wei
  • Yu Xu
  • Wuji Peng
  • Hongbo Su
  • Hong Li
  • Daren Yu
Regular Article
  • 73 Downloads
Part of the following topical collections:
  1. Topical Issue: Physics of Ion Beam Sources

Abstract

This study adopts double permanent magnetic rings and four permanent magnetic rings to form two symmetrical magnetic peaks and two asymmetrical magnetic peaks in the channel of a Hall thruster, and uses a 2D-3V PIC-MCC model to analyze the influence of magnetic strength on the discharge characteristic and performance of Hall thrusters with an intermediate electrode and double-peaked magnetic field. As opposed to the two symmetrical magnetic peaks formed by double permanent magnetic rings, increasing the magnetic peak value deep within the channel can cause propellant ionization to occur; with the increase in the magnetic peak deep in the channel, the propellant utilization, thrust, and anode efficiency of the thruster are significantly improved. Double-peaked magnetic field can realize separate control of ionization and acceleration in a Hall thruster, and provide technical means for further improving thruster performance.

Graphical abstract

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Copyright information

© EDP Sciences, SIF, Springer-Verlag GmbH Germany 2017

Authors and Affiliations

  • Yongjie Ding
    • 1
    • 2
  • Peng Li
    • 1
  • Hezhi Sun
    • 1
  • Liqiu Wei
    • 1
    • 2
  • Yu Xu
    • 1
  • Wuji Peng
    • 1
  • Hongbo Su
    • 1
  • Hong Li
    • 1
    • 2
  • Daren Yu
    • 1
    • 2
  1. 1.Plasma Propulsion Lab, Institute of Advanced Power, Harbin Institute of TechnologyHarbinP.R. China
  2. 2.Electric Drive & Propulsion Technology Lab, Harbin Institute of TechnologyHarbinP.R. China

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