航天器环境工程2015，Vol.32Issue(4)：361-365,5.DOI:10.3969/j.issn.1673-1379.2015.04.004
天基激光清除空间碎片方案与可行性研究
Active removal of space debris by space-based laser system and its feasibility analysis
摘要
Abstract
In this paper, the principles of the laser-induced ablative driving and the space debris de-orbiting are discussed. The criteria of the active removal of space debris and two modes for de-orbiting are analyzed. Based on the above theories, three removal schemes are proposed, for removing debris around typical orbits at altitudes of 1200km, 800km and 500km. The requirements of the schemes and the technologies are compared, and it is shown that the active removal of space debris using the space-based laser system is feasible.关键词
天基激光/空间碎片清除/降轨清除模式/激光器系统/可行性分析Key words
space-based laser/space debris removal/de-orbiting mode/laser system/availability analysis分类
航空航天引用本文复制引用
杨武霖,牟永强,曹燕,于兆吉,徐坤博,龚自正..天基激光清除空间碎片方案与可行性研究[J].航天器环境工程,2015,32(4):361-365,5.基金项目
国家自然科学基金重点项目(编号11332002) （编号11332002）
