| 螺旋波电推进的搭载试验装置结构设计与分析 |
| |
| 引用本文： | 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,2014,31(6):594-598. |
| |
| 作者姓名： | 王俊峰 赵华 任琼英 徐焱林 毕研强 |
| |
| 作者单位： | 北京卫星环境工程研究所,北京,100094 |
| |
| 摘 要： | 螺旋波是未来空间电推进系统极具吸引力的电离源之一，逐渐受到国内外高度关注。为进一步验证其可靠性，考虑进行螺旋波电推进的搭载试验。文章对螺旋波电推进搭载试验装置的支撑结构进行了详细的设计与分析，并采用有限元软件进行了力学计算，以验证结构设计的合理性。
|
| 关 键 词： | 螺旋波 电推进 搭载装置 结构设计 |
| 收稿时间： | 6/4/2014 12:00:00 AM |
| 修稿时间： | 2014/11/19 0:00:00 |
Design and analysis of the structure of helicon wave electric propulsion experiment system piggybacked on satellite |
| |
| Wang Junfeng,Zhao Hu,Ren Qiongying,Xu Yanlin,Bi Yanqiang.Design and analysis of the structure of helicon wave electric propulsion experiment system piggybacked on satellite[J].Spacecraft Environment Engineering,2014,31(6):594-598. |
| |
| Authors: | Wang Junfeng Zhao Hu Ren Qiongying Xu Yanlin Bi Yanqiang |
| |
| Institution: | Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China |
| |
| 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. |
| |
| Keywords: | helicon wave electric propulsion piggyback load structural design |
| 本文献已被 维普 万方数据 等数据库收录！ |
| 点击此处可从《航天器环境工程》浏览原始摘要信息 |
| 点击此处可从《航天器环境工程》下载免费的PDF全文 |
|
