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放电电压和屏栅电压对离子推力器性能的影响

王雨玮 任军学 吉林桔 汤海滨

中国空间科学技术2016,Vol.36Issue(1):77-84,8.
中国空间科学技术2016,Vol.36Issue(1):77-84,8.DOI:10.3780/j.issn.1000-758X.2016.0014

放电电压和屏栅电压对离子推力器性能的影响

Effects of discharge voltage and screen grid voltage on performance of ion thruster

王雨玮 1任军学 1吉林桔 2汤海滨1

作者信息

  • 1. 北京航空航天大学 宇航学院,北京 100191
  • 2. 北京动力机械研究所,北京 100074
  • 折叠

摘要

Abstract

The effects of discharge voltage and screen grid voltage changing to working performance of a 6 cm Kaufman ion thruster were studied by combination of experiments and numerical simulation. In these experiments, the argon was used as propellant for the ion thruster,and many groups of data were gathered. Furthermore, based on Goebel's theory model,the effects of discharge voltage changing on beam current and propellant efficiency were simulated.And the particle in cell Monte-Carlo collide (PIC-MCC)theory was used to simulate the effects of screen voltage on beam current,propellant efficiency and acceleration grid current. Experiments and numerical simulation drew the same conclusions. When discharge voltage increases,ion beam current and propellant utilization efficiency tend to be stable after a corresponding increase.A similar beam electric current and propellant utilization efficiency changing pattern is observed when the screen grid voltage is increased, but acceleration grid voltage tends to be stable after a corresponding decrease.This study can provide a reference for increasing multi-modes ion thrusters'performance.

关键词

离子推力器/多模式/放电电压/屏栅电压/氩气

Key words

ion thruster/multi-modes/discharge voltage/screen grid voltage/argon

分类

航空航天

引用本文复制引用

王雨玮,任军学,吉林桔,汤海滨..放电电压和屏栅电压对离子推力器性能的影响[J].中国空间科学技术,2016,36(1):77-84,8.

基金项目

北京市高等教育 "青年英才"计划 (YETP1129) (YETP1129)

中国空间科学技术

OA北大核心CSCDCSTPCD

1000-758X

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