深空探测学报2018，Vol.5Issue(4)：367-373,7.DOI:10.15982/j.issn.2095-7777.2018.04.007
大功率轨道转移航天器全电推进系统研究
Study on High Power All-Electric Propulsion System for Spacecraft Orbit Transfer
汤章阳 1周成 2韩冬 1马雪 2陈涛1
作者信息
- 1. 北京控制工程研究所,北京 100190
- 2. 北京市绿色高效能空间推进工程中心,北京 100190
- 折叠
摘要
Abstract
Compared with chemical propulsion,the application electric propulsion system in spacecraft can save the amount of propellant,which is able to significantly reduce the launch mass or allow more payloads to the target. In this paper,the research on high power electric thrusters in the world is investigated. An electric propulsion systemis designed for the near-earth spacecraft orbit transfer. Several schemes are compared with different thruster performances. At last,the suggestions are proposed for developing high power electric thruster and propulsion system in China.关键词
大功率/电推进系统/轨道转移Key words
high power/electric propulsion/orbit transfer分类
航空航天引用本文复制引用
汤章阳,周成,韩冬,马雪,陈涛..大功率轨道转移航天器全电推进系统研究[J].深空探测学报,2018,5(4):367-373,7.
