| 离子推力器热真空试验研究 |
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| 引用本文： | 郑茂繁,江豪成,顾 左,马诗龙.离子推力器热真空试验研究[J].航天器环境工程,2008,25(2):169-172. |
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| 作者姓名： | 郑茂繁 江豪成 顾 左 马诗龙 |
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| 作者单位： | 兰州物理研究所,兰州,730000 |
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| 摘 要： | 为了验证离子推力器的空间环境适应性,对离子推力器进行了热真空试验研究,确定了热真空试验的温度。试验结果表明:离子推力器在热真空环境中,启动和工作正常,性能稳定,满足空间环境要求。
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| 关 键 词： | 离子推力器 环境试验 热真空 |
| 收稿时间： | 2007/11/12 0:00:00 |
| 修稿时间： | 2007/11/20 0:00:00 |
The thermal vacuum test on ion thruster |
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| Zheng Maofan,Jiang Haocheng,Gu Zuo and Ma Shilong.The thermal vacuum test on ion thruster[J].Spacecraft Environment Engineering,2008,25(2):169-172. |
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| Authors: | Zheng Maofan Jiang Haocheng Gu Zuo and Ma Shilong |
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| Institution: | Lanzhou Institute of Physics;Lanzhou Institute of Physics;Lanzhou Institute of Physics;Lanzhou Institute of Physics |
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| Abstract: | The high and low temperature vacuum experiments were carried out for validating space environment applicability of ion thruster. The results show that ion thruster can start and operate naturally under the vacuum environment of high and low temperature with stable performance and can meet the requirement of space environment. |
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| Keywords: | ion thruster environmental test thermal vacuum |
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