推进技术 ›› 1998, Vol. 19 ›› Issue (3): 21-26.

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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   

  1. 西北工业大学航天工程学院;西北工业大学航天工程学院;西北工业大学航天工程学院;西北工业大学航天工程学院
  • 发布日期:2021-08-15
  • 基金资助:
    国家“八六三”基金

EXPLORATORY RESEARCH ON PRINCIPLE AND UTILITYOF MICROWAVE PLASMA THRUSTER(MPT)

  1. Collof Astronautics,Northwestern Polytechnical Univ,Xi′an,710072;Collof Astronautics,Northwestern Polytechnical Univ,Xi′an,710072;Collof Astronautics,Northwestern Polytechnical Univ,Xi′an,710072;Collof Astronautics,Northwestern Polytechnical Univ,Xi′an,710072
  • Published:2021-08-15

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

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