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基于水推进剂的脉冲等离子体推力器数值模拟

王司宇 刘向阳 杨磊 武志文 成跃 王宁飞

高电压技术2013,Vol.39Issue(7):1680-1686,7.
高电压技术2013,Vol.39Issue(7):1680-1686,7.DOI:10.3969/j.issn.1003-6520.2013.07.021

基于水推进剂的脉冲等离子体推力器数值模拟

Numerical Simulation of Pulsed Plasma Thruster Based on Water Propellant

王司宇 1刘向阳 1杨磊 1武志文 1成跃 1王宁飞1

作者信息

  • 1. 北京理工大学宇航学院,北京100081
  • 折叠

摘要

Abstract

In order to reveal the specific ablation mechanism of water propellant pulsed plasma thruster (WP-PPT)and to overcome critical obstacles in its application,we simulated and investigated the working process of WP-PPT by an ablation model for WP-PPT.The simulation results were compared with the experimental results obtained by researchers in University of Tokyo.The comparison indicated that,because some water was gasified before being ignited and some was remained in the electrode area after discharge,the experimental results were different from the simulation ones.However,with the working parameters of prototype and a quality percentage of propellant participating in discharge of 20 %,the simulation performances could fit the experimental results well.The impulse bit,specific impulse and energy conversion efficiencies in the simulation results were 74 μN · s,1114 s,and 15.2%,respectively.According to analysis of the experiment,it was estimated that about 32% of propellant participated in discharge,which was close to the simulation.We further proposed that developing injector which was able to respond rapidly and jet uniformly would improve the performance of WP-PPT.

关键词

脉冲等离子体推力器/水推进剂/烧蚀模型/烧蚀质量/元冲量/喷注器

Key words

pulsed plasma thruster/water propellant/ablation model/ablation mass/impulse bit/injector

引用本文复制引用

王司宇,刘向阳,杨磊,武志文,成跃,王宁飞..基于水推进剂的脉冲等离子体推力器数值模拟[J].高电压技术,2013,39(7):1680-1686,7.

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