Status and prospect of Hall thruster of different thrust stages

被引：0
|
作者：
Liu Y. [1 ]
Zhang X. [1 ]
机构：
[1] School of Astronautics, Beihang University, Beijing
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2022年 / 37卷 / 12期
关键词：
Hall electric propulsion technology; Hall thruster; space thruster; thrust; thrust stage;
D O I：
10.13224/j.cnki.jasp.20220003
中图分类号：
学科分类号：
摘要：
Based on the introduction of the principle of Hall thruster，the influencing factors of Hall thruster thrust were deduced and analyzed，summarizing how to change Hall thruster thrust. The types of space missions applicable to different thrust levels，such as µN-level level，mN-level and N-level were summarized. The models of Hall thrusters at home and abroad were classified according to three levels，and the development and trend of each series of models of the three thrust levels were sorted out and analyzed respectively. The technical bottleneck and development trend were summarized and analyzed. Hall thrusters of various thrust stages were comprehensively and systematically reviewed. The results indicated that the mN-level was the most mature. With more abundant types of space missions，the µN-level level and N-level Hall thrusters had considerable development potential. The key technologies for the development of Hall Thrusters in each thrust stage were prospected. The results suggested that Hall Thrusters should improve the overall performance，expand the thrust coverage，strengthen the multi-mode working ability，develop hollow cathode and explore different propellants，thus providing a reference for the further development of Hall electric propulsion. © 2022 BUAA Press. All rights reserved.
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页码：2782 / 2796
页数：14
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