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现代小卫星的微推进系统
引用本文:林来兴.现代小卫星的微推进系统[J].航天器工程,2010,19(6):13-20.
作者姓名:林来兴
作者单位:北京控制工程研究所,北京100080
摘    要:现代小卫星,发展迅速,不仅要姿态控制,还要轨道控制,甚至要有轨道机动能力。为此,必须开发研究与其相应的微推进系统。文章首先研究现有推进系统的技术性能;提出对微推进系统的要求;给出适应小卫星的微推进系统,有四个种类,近20个微推进器;最后提出选择微推进器的原则和建议。

关 键 词:小卫星  微推进系统  化学微推进器  电微推进器  数字固体微推进器

Micro-propulsion System for Modern Small Satellites
LIN Laixing.Micro-propulsion System for Modern Small Satellites[J].Spacecraft Engineering,2010,19(6):13-20.
Authors:LIN Laixing
Institution:LIN Laixing (Beijing Institute of Control Engineering,Beijing 100080,China)
Abstract:Modern small satellites are rapidly developed and widely application. The small satellites need not only attitude control,but also orbit control or even orbit maneuver function . Therefore,we should research and develop the corresponding micro-propulsion system. This paper studies the technology performances of current propulsion system,suggests micro-propulsion system requirements,gives micro-propulsion system adaptable to small satellites,including four species and about 20 micro-thrusters,and finally gives selection principles and recommendation of micro-thrusters.
Keywords:small satellite  micro-propulsion system  chemical micro-thruster  electric micro-thruster  digital solid micro-thruster
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