| 小型微波等离子推力器研究 |
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| 引用本文： | 何洪庆,毛根旺,杨涓,唐金兰,韩先伟.小型微波等离子推力器研究[J].航空学报,2003,24(5):391-394. |
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| 作者姓名： | 何洪庆 毛根旺 杨涓 唐金兰 韩先伟 |
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| 作者单位： | 西北工业大学,航天学院,陕西,西安,710072 |
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| 基金项目： | 国防基础研究(J1400D001)，国家863 2计划(863 2 2 5 |
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| 摘 要： | 介绍约100W 功率微波等离子推力器的系统结构, 谐振模式, 电磁场分布, 电磁场、等离子体和流场的耦合, 喷管中的等离子体复合流动, 真空羽流, 原理实验样机性能及应用前景。
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| 关 键 词： | 电推进 微波等离子推力器 电磁场 流场 轨道转移 |
| 文章编号： | 1000-6893(2003)05-0391-04 |
| 修稿时间： | 2003年6月3日 |
Study of Small Microwave Plasma Thruster |
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| HE Hong-qing,MAO Gen-wang,YANG Juan,TANG Jin-lan,HAN Xian-wei.Study of Small Microwave Plasma Thruster[J].Acta Aeronautica et Astronautica Sinica,2003,24(5):391-394. |
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| Authors: | HE Hong-qing MAO Gen-wang YANG Juan TANG Jin-lan HAN Xian-wei |
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| Institution: | College of Astronautics; Northwestern Polytechnical University; Xi'an 710072; China |
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| Abstract: | Small pr inciple pro to type of Microwave Plasma Thruster ( MPT) has been tested. Follow ing is introducedabout the 100W pow er MPT: system construction, r esonance mo de, distribution of electromagnetic field, couplingbetween electromag netic field, plasma and flow field, complex flow of plasma in nozzle, vacuum plume, performance of prototype and applicat ion prospect of MPT. Some coupled formulae, such as the N-S, Maxwell and Sahaequat ions, ar e introduced when studying the electr omag netic field, t he coupled plasma flow field in r esonance cavity,and the complex flow in nozzle. |
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| Keywords: | electric propulsion microwave plasma thruster electric-magnet field flow field orbit transfer |
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