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表面带电对航天员出舱活动的影响及对策分析
引用本文:梁晓锋,周东,秦晓刚,刘业楠.表面带电对航天员出舱活动的影响及对策分析[J].航天器环境工程,2014,31(2):168-172.
作者姓名:梁晓锋  周东  秦晓刚  刘业楠
作者单位:1. 中国空间技术研究院 载人航天总体部, 北京 100094;2. 兰州空间技术物理研究所, 兰州 730000;3. 北京卫星环境工程研究所, 北京 100094
摘    要:根据我国某载人航天器在轨飞行时的空间环境和航天器表面带电的机理,对航天器表面带电进行了仿真,并对结构切割地磁场的感应电势进行计算。在此基础上,分析了表面带电对航天员出舱的影响,以及出舱安全性防护措施,计算出主动电位控制系统最大发射电流。研究结果可为航天员出舱安全防护提供参考。

关 键 词:表面带电  航天员出舱活动  感应电势  高压太阳电池阵  带电防护
收稿时间:2013/11/14 0:00:00
修稿时间:2014/3/21 0:00:00

Influences of surface charging on astronaut EVA and countermeasures
Liang Xiaofeng,Zhou Dong,Qin Xiaogang,Liu Ye''nan.Influences of surface charging on astronaut EVA and countermeasures[J].Spacecraft Environment Engineering,2014,31(2):168-172.
Authors:Liang Xiaofeng  Zhou Dong  Qin Xiaogang  Liu Ye'nan
Institution:1. Institute of Manned Space System Engineering, China Academy of Space Technology, Beijing 100094, China;2. Lanzhou Institute of Space Technology and Physics, Lanzhou 730000, China;3. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China
Abstract:Based on the space environment of manned spacecraft, this paper analyzes the surface charging mechanism. Simulations are conducted to calculate the charging potential as the structure passes through the earth magnet field, to reveal the influence of the surface charging on astronaut extravehicular activities. Some security protecting measures are proposed for the extravehicular activities(EVA). The active potential control approach is proposed to solve the high transmitter current and provide a design guidance for the EVA safety.
Keywords:surface charging  astronaut EVA  induction potential  high voltage solar array  charging protection
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