航天器环境工程2011，Vol.28Issue(5)：440-445,6.DOI:10.3969/j.issn.1673-1379.2011.05.007
电推进羽流与航天器相互作用的研究现状与建议
A review of the researches of interaction between electric propulsion plume and spacecraft
摘要
Abstract
The electric propulsion can provide a substantial mass saving as compared to the conventional chemical engine. It has been widely used for the station keeping and the primary propulsion of geosynchronous satellites in deep space missions. The plume induced by electric propulsion thruster is quite different from that produced by the chemical engine. The interactions between the electric propulsion plume and the spacecraft must be considered by designers. In this paper,the effects of the electric propulsion plume on the spacecraft are discussed. The related ground simulation test,in-flight test and software simulation are reviewed. Some suggestions are made for the research work in this field in China.关键词
电推进羽流/地面模拟试验/飞行试验/软件仿真Key words
electric propulsion plume/ground simulation test/in-flight test/software simulation分类
航空航天引用本文复制引用
刘磊,张庆祥,王立,薛玉雄,杨生胜,安恒..电推进羽流与航天器相互作用的研究现状与建议[J].航天器环境工程,2011,28(5):440-445,6.基金项目
国家“863”计划资助项目(编号:2010AA122206) （编号:2010AA122206）
