Effects of Magnetic Shielding Configuration on Discharge Characteristics and Performance of a 60 mm-Diameter Low-Power Hall Thruster

IF 0.9 Q3 ENGINEERING, AEROSPACE Journal of Aerospace Technology and Management Pub Date : 2021-05-21 DOI:10.1590/JATM.V13.1223
W. Guo, Jun Gao, Zuo Gu, Ning Guo, Mingfang Sun
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Abstract

Lifetime is a main factor restraining the application of low-power Hall thruster. Magnetic shielding configuration is regarded as a promising method to prolong the lifespan of Hall thruster. Aiming to demonstrate the feasibility and effectiveness of magnetic shielding configuration applying on low-power Hall thruster, a 60-mm diameter Hall thruster in partial magnetic shielding configuration was designated. Both the numerical and experimental methods were used to investigate the discharge characteristics of the Hall thruster and help understand the mechanism behind. The maximum anode efficiency was achieved as high as 29.7% with 1.7 mg·s–1 anode mass flow and 320 V discharge voltage. To evaluate the effectiveness of the magnetic shielding used for low-power Hall thruster, a 2000 h lifetime test has been carried out and the results indicate that the erosion rate has been decreased below 0.2 μm·h–1.
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磁屏蔽结构对60mm直径小功率霍尔推力器放电特性和性能的影响
寿命是制约低功率霍尔推力器应用的主要因素。磁屏蔽结构被认为是一种很有前途的延长霍尔推进器寿命的方法。为了验证磁屏蔽结构应用于小功率霍尔推进器的可行性和有效性,设计了一种60mm直径的部分磁屏蔽霍尔推进器。采用数值和实验相结合的方法研究了霍尔推力器的放电特性,有助于了解其背后的机理。当阳极质量流量为1.7 mg·s-1,放电电压为320 V时,阳极效率最高可达29.7%。为了评价磁屏蔽在小功率霍尔推进器上的有效性,进行了2000 h寿命试验,结果表明,磁屏蔽的腐蚀速率降低到0.2 μm·h - 1以下。
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CiteScore
2.00
自引率
0.00%
发文量
16
审稿时长
20 weeks
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