航天器环境工程Issue(6)：594-598,5.DOI:10.3969/j.issn.1673-1379.2014.06.005
螺旋波电推进的搭载试验装置结构设计与分析
Design and analysis of the structure of helicon wave electric propulsion experiment system piggybacked on satellite
王俊峰 1赵华 1任琼英 1徐焱林 1毕研强1
作者信息
- 1. 北京卫星环境工程研究所，北京 100094
- 折叠
摘要
Abstract
The helicon wave, as one of the attractive ionization sources for the space electric propulsion in the future, is attracting more and more attention domestically and abroad. The piggyback experiment on a satellite for the helicon wave electric propulsion is used to validate the technology. In this paper, the structure, with the main part bearing the load, is designed and analyzed, followed by a mechanical calculation by the finite element method(FEM) to validate the rationality and reliability of the design.关键词
螺旋波/电推进/搭载装置/结构设计Key words
helicon wave/electric propulsion/piggyback load/structural design分类
航空航天引用本文复制引用
王俊峰,赵华,任琼英,徐焱林,毕研强..螺旋波电推进的搭载试验装置结构设计与分析[J].航天器环境工程,2014,(6):594-598,5.
