高技术通讯2001，Vol.11Issue(4)：72-75,4.
微流星及空间碎片高速撞击航天器风险度分析
Risk Analysis of Meteoroid and Space Debris
High-velocity Impact on Spacecraft
摘要
Abstract
The risk analysis approach has been illustrated. Taking cylinder spacecraft in LEO as an example, the effects of various shield configurations, flight attitudes, thickness of shield bumper and operation duration etc. on meteoroid and space debris impact probability of no perforation have been performed by using risk analysis program. The analysis results were presented.关键词
航天器/微流星/空间碎片/高速撞击/风险度分析分类
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张伟,庞宝君,夏仁波,张泽华..微流星及空间碎片高速撞击航天器风险度分析[J].高技术通讯,2001,11(4):72-75,4.
