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High-voltage discharge characteristics of a hybrid-wall Hall thruster with an aft-loaded magnetic field

  • Harbin Institute of Technology
  • Ministry of Industry and Information Technology
  • Beijing Aerospace Technology Research Institute
  • CAS - Beijing Institute of Control Engineering

Research output: Contribution to journalArticlepeer-review

Abstract

Hall thrusters generally use a U-shaped insulated wall to form an annular discharge channel. As high-power and high-specific-impulse Hall thrusters develop, the disadvantages of this conventional topology—in terms of material and mechanical strength, processing, and manufacturing—are gradually being exposed. Therefore, in this study, a new wall material was employed, and its effects were investigated numerically and experimentally. A boron nitride ceramic wall was retained in the strong discharge area owing to its excellent secondary electron emission characteristics; while a metallic wall was applied upstream of the channel, forming a segmented hybrid wall. A Hall thruster with an aft-loaded magnetic field, which offers a long lifetime, was adopted for this study. The particle-in-cell simulation shows that the length of the metallic wall has a significant impact on thruster performance. The same trend was observed in the experiments. Under the optimal metallic wall length, the anode efficiency is improved by approximately 4% compared to that of the ceramic-wall-only case. The physics involved is analyzed and qualified by comparing the simulated and measured results. The findings of this study provide valuable guidance for the optimal design of high-power, high-specific-impulse Hall thrusters.

Original languageEnglish
Pages (from-to)214-225
Number of pages12
JournalActa Astronautica
Volume203
DOIs
StatePublished - Feb 2023

Keywords

  • Aft-loaded magnetic field
  • Electric propulsion
  • Hall thruster
  • High voltage
  • Wall material

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