TY - JOUR
T1 - Influence of cathode position on the performance of a low-power planar Hall thruster
AU - Kong, Weiyi
AU - Wang, Weizong
AU - Liu, Ran
AU - Li, Yifei
AU - Liu, Wei
AU - Zhang, Guangchuan
N1 - Publisher Copyright:
© 2026 IOP Publishing Ltd. All rights, including for text and data mining, AI training, and similar technologies, are reserved.
PY - 2026/4/3
Y1 - 2026/4/3
N2 - 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.
AB - 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.
KW - cathode position
KW - coupling relationship
KW - oscillation characteristic
KW - performance
KW - planar Hall thruster
KW - total efficiency
UR - https://www.scopus.com/pages/publications/105034716622
U2 - 10.1088/1402-4896/ae54e4
DO - 10.1088/1402-4896/ae54e4
M3 - 文章
AN - SCOPUS:105034716622
SN - 0031-8949
VL - 101
JO - Physica Scripta
JF - Physica Scripta
IS - 13
M1 - 135506
ER -