微型化阳极层推力器数值模拟与性能实验*

Numerical Simulation and Experimental Research on Miniaturized Anode Layer Thruster

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doi:10.13385/j.cnki.vacuum.2023.04.07

Abstract: In this paper, particle grid combined with Monte Carlo collision method was used to simulate the miniaturized anode layer Hall thruster. Meanwhile, the discharge experiment of the miniaturized anode layer Hall thruster was carried out to evaluate its performance. The results show that the discharge of the miniaturized anode layer thruster is stable, and the ion beam presents a bunched mode. The discharge voltage range is 300~1100V, the specific impulse range is 234~2047s, and the thrust range is 0.5~5.4mN. This study can provide certain data support for further optimization design of high efficiency, light mass and high performance micro anode layer Hall thruster.

Key words: anode layer thruster, microminiaturization, numerical simulation, work performance

CLC Number: V19;TB79

LI Ping-chuan, XU Li, ZHAO Jie, ZHANG Fan, XIONG Si-wei, JIAN Yi, ZHANG Zheng-hao, TANG De-li. Numerical Simulation and Experimental Research on Miniaturized Anode Layer Thruster[J].VACUUM, 2023, 60(4): 36-41.

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