| 大功率轨道转移航天器全电推进系统研究 |
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| 作者姓名： | 汤章阳 周成 韩冬 马雪 陈涛 |
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| 作者单位： | 北京控制工程研究所, 北京 100190;北京市绿色高效能空间推进工程中心, 北京 100190,北京控制工程研究所, 北京 100190;北京市绿色高效能空间推进工程中心, 北京 100190,北京控制工程研究所, 北京 100190;北京市绿色高效能空间推进工程中心, 北京 100190,北京控制工程研究所, 北京 100190;北京市绿色高效能空间推进工程中心, 北京 100190,北京控制工程研究所, 北京 100190;北京市绿色高效能空间推进工程中心, 北京 100190 |
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| 摘 要： | 采用基于电推进的空间运输系统(转移级)完成使命,相对于采用化学推进可节省大量的推进剂,能够显著降低航天器的发射重量或者把更多的有效载荷送达探测目标地。调研了国外大功率电推力器的研究情况,针对近地空间的大功率轨道转移航天器任务需求,给出了电推进系统方案设计,并对采用不同性能指标推力器的多种方案进行对比,得到综合最优的方案。最后针对我国电推进技术发展现状,给出了我国大功率电推力器的关键技术和发展建议。
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| 关 键 词： | 大功率 电推进系统 轨道转移 |
| 收稿时间： | 2018/2/1 0:00:00 |
| 修稿时间： | 2018/6/3 0:00:00 |
Study on High Power All-Electric Propulsion System for Spacecraft Orbit Transfer |
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| Authors: | TANG Zhangyang ZHOU Cheng HAN Dong MA Xue and CHEN Tao |
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| Institution: | BeijingInstitute of Control Engineering, Beijing 100190, China;Beijing Engineering Center of Green High-efficience Space Propulsion, Beijing 100190, China,BeijingInstitute of Control Engineering, Beijing 100190, China;Beijing Engineering Center of Green High-efficience Space Propulsion, Beijing 100190, China,BeijingInstitute of Control Engineering, Beijing 100190, China;Beijing Engineering Center of Green High-efficience Space Propulsion, Beijing 100190, China,BeijingInstitute of Control Engineering, Beijing 100190, China;Beijing Engineering Center of Green High-efficience Space Propulsion, Beijing 100190, China and BeijingInstitute of Control Engineering, Beijing 100190, China;Beijing Engineering Center of Green High-efficience Space Propulsion, Beijing 100190, China |
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| Abstract: | Compared with chemical propulsion,the application electric propulsion system in spacecraft can save the amount of propellant,which is able to significantly reduce the launch mass or allow more payloads to the target. In this paper,the research on high power electric thrusters in the world is investigated. An electric propulsion systemis designed for the near-earth spacecraft orbit transfer. Several schemes are compared with different thruster performances. At last,the suggestions are proposed for developing high power electric thruster and propulsion system in China. |
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| Keywords: | high power electric propulsion orbit transfer |
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