航天器带电及其表面电位主动控制技术发展现状
Present Situation of Active Control Technologies Concerning Spacecraft Charging and Its Surface Potential and Their Developments
代银松 1张希军 1罗健峰 2谷皓东3
作者信息
- 1. 军械工程学院静电与电磁防护研究所
- 2. 政治部,河北 石家庄 050003
- 3. 兰州大学大气科学学院,甘肃 兰州 730000
- 折叠
摘要
分析航天器表面带电机理和安全隐患,结合载人航天器结构实例分析等离子体和航天器作用过程及危害,阐述航天器表面电位主动控制技术发展及其应用情况,并对航天器表面电位主动控制技术的发展趋势作出预测,为进一步研究航天器表面电位主动控制技术提供参考.
Abstract
This paper analyses the charging mechanism of spacecraft surface and its corresponding security risks,and on the basis of the analysis of the action process and damage of plasma and spacecraft in the case of manned spacecraft, elaborates on potential active control technology development and application,and predicts the development trend of spacecraft surface potential active control technology,and provides technical reference for further studies in this respect.
关键词
航天器/带电机理/电位主动控制Key words
spacecraft/charged mechanism/potential active control引用本文复制引用
出版年
2017
NETL
NSTL
维普
万方数据