| 电推进羽流与航天器相互作用的研究现状与建议 |
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| 引用本文： | 刘 磊,张庆祥,王 立,薛玉雄,杨生胜,安 恒.电推进羽流与航天器相互作用的研究现状与建议[J].航天器环境工程,2011,28(5):440-445. |
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| 作者姓名： | 刘 磊 张庆祥 王 立 薛玉雄 杨生胜 安 恒 |
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| 作者单位： | 北京空间飞行器总体设计部;兰州物理研究所真空低温技术与物理重点实验室; |
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| 基金项目： | 国家“863”计划资助项目(编号:2010AA122206) |
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| 摘 要： | 电推进与传统的化学推进相比可以节约大量推进剂质量,被广泛用作地球同步轨道卫星南北位置保持和深空探测等任务的主推进系统.电推进器工作时产生的羽流与传统的化学推进器羽流有显著区别,电推进羽流对航天器的影响是进行卫星电推进器系统设计时需要重点关注的问题.文章讨论了电推进羽流对航天器的主要影响,介绍了国外在地面模拟试验、空间飞...
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| 关 键 词： | 电推进羽流 地面模拟试验 飞行试验 软件仿真 |
| 收稿时间： | 2011/6/13 0:00:00 |
| 修稿时间： | 2011/6/21 0:00:00 |
A review of the researches of interaction between electric propulsion plume and spacecraft |
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| Liu Lei,Zhang Qingxiang,Wang Li,Xue Yuxiong,Yang Shengsheng and An Heng.A review of the researches of interaction between electric propulsion plume and spacecraft[J].Spacecraft Environment Engineering,2011,28(5):440-445. |
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| Authors: | Liu Lei Zhang Qingxiang Wang Li Xue Yuxiong Yang Shengsheng and An Heng |
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| Affiliation: | Liu Lei1,Zhang Qingxiang1,Wang Li1,Xue Yuxiong2,Yang Shengsheng2,An Heng2(1.Beijing Institute of Spacecraft System Engineering,Beijing 100094,China,2.Key Laboratory of Science and Technology on Vacuum & Cryogenics Technology and Physics,Lanzhou Institute of Physics,Lanzhou 730000,China) |
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| Abstract: | The electric propulsion can provide a substantial mass saving as compared to the conventional chemical engine.It has been widely used for the station keeping and the primary propulsion of geosynchronous satellites in deep space missions.The plume induced by electric propulsion thruster is quite different from that produced by the chemical engine.The interactions between the electric propulsion plume and the spacecraft must be considered by designers.In this paper,the effects of the electric propulsion plume... |
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| Keywords: | electric propulsion plume ground simulation test in-flight test software simulation |
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