多任务模式电推进技术  

Multitask Mode Electric Propulsion Technologies

作　　者：温正[1] 王敏[1] 仲小清[1] 

机构地区：[1]中国空间技术研究院,北京100094

出　　处：《航天器工程》2014年第1期118-123,共6页Spacecraft Engineering

摘　　要：调研了多任务模式电推进技术在地球静止轨道卫星和深空探测器中的应用情况,电推进技术的应用由南北位置保持任务模式逐步向南北位置保持和轨道转移等多任务模式发展;总结了多任务模式电推进技术在功率需求、比冲、推力等方面的技术特点;从卫星平台技术、推力器技术、可变功率电源转换及控制技术、可变流量调节技术,以及多自由度、大角度矢量调节技术等方面,分析了多任务模式电推进在工程应用中要解决的关键技术。The applications of multitask mode electric propulsion technologies in GEO satellites and deep space probes are introduced, and the electric propulsion technologies are used from single task mode of north/south-station keeping of orbit to multitask mode of north/south-station keep- ing of orbit and orbit-transfer. The functions of multitask mode electric propulsion technologies such as power demand, specific impulse, and thrust are summarized. Key techniques for multi- task mode electric propulsion technologies are discussed, including satellite platform, thruster, conversion and control of variable power supply, variable flow adjustment, and adjustment of multi-freedom and large angle vector.

关 键 词：卫星 电推进技术 多任务模式 

分 类 号：V439.4[航空宇航科学与技术—航空宇航推进理论与工程]