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多任务模式电推进技术
引用本文:温正,王敏,仲小清.多任务模式电推进技术[J].航天器工程,2014(1):128-133.
作者姓名:温正  王敏  仲小清
作者单位:中国空间技术研究院;
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。

关 键 词:卫星  电推进技术  多任务模式

Multitask Mode Electric Propulsion Technologies
WEN Zheng,WANG Min,ZHONG Xiaoqing.Multitask Mode Electric Propulsion Technologies[J].Spacecraft Engineering,2014(1):128-133.
Authors:WEN Zheng  WANG Min  ZHONG Xiaoqing
Institution:(China Academy of Space Technology, Beijing 100094, China)
Abstract: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.
Keywords:satellite  electric propulsion technology  multitask mode
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