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Influence of cathode position on the performance of a low-power planar Hall thruster

  • Beihang University
  • State Key Laboratory of High-Efficiency Reusable Aerospace Transportation Technology
  • Beijing Key Laboratory of System Design for Reusable Launch Vehicle

Research output: Contribution to journalArticlepeer-review

Abstract

The planar Hall thruster (PHT) is a novel Hall thruster with an exposed ionization region, enhancing coupling between cathode and anode, though the enhanced coupling in PHT is insufficiently studied. This study experimentally investigates the effects of the coupling relationship—regulated primarily through cathode positioning—on the propulsion performance and oscillations of the PHT. The net magnetic region traversed by electrons initially expands and then contracts with increasing cathode radial position (rc), resulting in performance that first declines before slightly recovering or stabilizing. Increasing the cathode axial position (zc) reduces the net magnetic region, thereby optimizing the coupling relationship, lowering the coupling voltage (Vc) and ultimately improving performance. By appropriately adjusting rc and zc, thrust can be increased by up to 38.4% (from 3.65 to 5.05 mN) and 40.55% (from 3.97 to 5.58 mN) respectively. Increasing zc can compress the beam half-angle, which decreases from 70.95° to 65.71°. The performance is also significantly affected by the cathode flow. The more active participation of cathode flow in discharge at smaller rc leads to a deviation between the rc for peak performance and that for Vc. Within the cathode flow range of 1~4 sccm (anode flow fixed at 5 sccm), the variation in total efficiency with cathode flow rate exhibits a strong dependence on cathode position. Cathode position also influences discharge oscillation. At zc < 30 mm, discharge oscillation is enhanced by the cathode flow, while for zc > 56 mm, oscillation decreases with increasing rc because of reduced electron energy. By optimizing the cathode position, the discharge oscillation can be reduced by up to 56.3%. Adjusting rc and zc at a fixed cathode flow can reduce the beam divergence and discharge oscillation while maintaining relatively high performance. This work provides valuable insights for optimizing cathode parameters in PHTs.

Original languageEnglish
Article number135506
JournalPhysica Scripta
Volume101
Issue number13
DOIs
StatePublished - 3 Apr 2026

Keywords

  • cathode position
  • coupling relationship
  • oscillation characteristic
  • performance
  • planar Hall thruster
  • total efficiency

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