| 脉冲等离子体源控制航天器表面充电电位的研究 |
| |
| 引用本文： | 鲁文涛,蒋远大,张志远,吴汉基.脉冲等离子体源控制航天器表面充电电位的研究[J].航天器工程,2011,20(5):116-124. |
| |
| 作者姓名： | 鲁文涛 蒋远大 张志远 吴汉基 |
| |
| 作者单位： | 1. 中国科学院研究生院,北京,100190
2. 中国科学院空间科学与应用研究中心,北京,100190 |
| |
| 摘 要： | 在空间环境运行的航天器存在表面充电现象,而航天器表面充电引发的静电放电是导致航天器异常及故障的重要原因之一。因此,在航天器设计和应用中,必须对航天器表面电位采取必要的控制和防护措施。文章介绍了用脉冲等离子体源进行航天器表面充电电位主动控制的研究。通过模拟实验和实验数据分析,证实了用脉冲等离子体源能有效地控制航天器表面充...
|
| 关 键 词： | 航天器 脉冲等离子体源 表面充电电位的主动控制 模拟实验 控制效率 |
Study on Active Control of Spacecraft Surface Charging Potential Based on the Pulsed Plasma Source |
| |
| LU Wentao, JIANG Yu,a ZHANG Zhiyuan WU Hanji.Study on Active Control of Spacecraft Surface Charging Potential Based on the Pulsed Plasma Source[J].Spacecraft Engineering,2011,20(5):116-124. |
| |
| Authors: | LU Wentao JIANG Yu a ZHANG Zhiyuan WU Hanji |
| |
| Institution: | LU Wentao1,2 JIANG Yuanda2 ZHANG Zhiyuan2 WU Hanji2(1 Graduate School of Chinese Academy of Sciences,Beijing 100190,China) (2 Center for Space Science & Applied Research,Chinese Academy of Sciences,China) |
| |
| Abstract: | There is surface charging when a spacecraft operates in the space environment.The electrostatic discharge induced by spacecraft surface charging is an important cause of spacecraft anomalies and failures.Therefore,we must take measures to control the surface potential of the spacecraft when we design and apply spacecraft.This paper presents the investigation of the active control of spacecraft surface charging potential by using a pulsed plasma source.Through simulation experiments and theoretical analysis,... |
| |
| Keywords: | spacecraft pulse plasma source active control of surface charging potential simulation experiment control efficiency |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
