全电推进卫星平台现状与进展  

THE REVIEW OF ALL-ELECTRIC PROPULSION PLATFORM ON SATELLITE

作　　者：魏冰洁[1] 孙小菁[1] 王小永[1] 

机构地区：[1]兰州空间技术物理研究所真空技术与物理重点实验室,兰州730000

出　　处：《真空与低温》2016年第5期301-305,310,共6页Vacuum and Cryogenics

摘　　要：全电推进技术的应用能够大幅缩减卫星推进剂携带量,增加有效载荷,是降低商业通信卫星研制及发射综合费用赢得市场的重要途径。在调研国内外全电推进平台的基础上,给出全电推进早期发展历史、现阶段技术特点、研究现状和未来发展趋势,为未来我国全电推进平台的开发研制提供有价值的参考。The application of All-Electric Propulsion Platform allows fewer propellant and more payload on satellite,which is an important approach to lower the research and launch costs of commercial communication satellites. Base on the investigation about the development of All-Electric Propulsion Platform,this paper introduces the early development history,current technical characteristics,research status and the prospects of All-Electric Propulsion Platform. It provides a reference on the development of All-Electric Propulsion Platform.

关 键 词：全电推进平台 研究现状 技术特点 

分 类 号：V439[航空宇航科学与技术—航空宇航推进理论与工程]