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微波等离子推进器(MPT)的应用探索研究
毛根旺, 何洪庆, 杨涓, 史韶莉
西北工业大学航天工程学院
摘要:
重点分析讨论了微波等离子推进器(MPT)的基本原理、结构特征和应用前景,并通过对已有理论与实验研究结果的分析,认为MPT是一种高比冲、长寿命的小推力动力装置,特别适合用作空间动力,进行航天器的轨道转移、姿态控制、位置保持、对接交会和星际航行。尽管MPT目前仍处于理论探索与实验研究阶段,但研究结果表明,它是前景十分诱人的新型空间动力系统。
关键词:  航天器推进  微波技术  等离子体推进  轨道机动发动机  卫星姿态控制
DOI:
分类号:V439.2
基金项目:国家“八六三”基金
EXPLORATORY RESEARCH ON PRINCIPLE AND UTILITY OF MICROWAVE PLASMA THRUSTER(MPT)
Mao Genwang, He Hongqing, Yang Juan, Shi Shaoli
Collof Astronautics,Northwestern Polytechnical Univ,Xi′an,710072
Abstract:
The primary principle configuration features and utility prospect of a new space propulsion system——microwave plasma thruster(MPT) were analysised and discussedAccording to the theoretical and experimental results achieved up to date,the conclusions can be drawn that MPT is a kind of advanced thruster with high specific impulse,long lifetime and low thrust,and especially fits for space propulsion such as orbit transfer,attitude cotrol,stationkeeping,docking and rendezious,and planetary missionsAlthough MPT is still at the theoretical and experimental exploratory research stage,it is very likely to be a new promising space propulsion system
Key words:  Spacecraft propulsion  Microwave technique  Plasma propulsion  Orbit maneuvering engine  Satellite attitude control