航天器轨道碎片撞击易损性模型研究

Chunmei Liu, Shunshan Feng, Xurong Zhang
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摘要

对宇宙飞船进行了研究。从环境、代表性结构、航空理论、损伤原理和存在特性等方面分析了航天器的易损性。在此基础上提出了碎片对双板的破坏类型。损伤类型包括局部穿孔和撕脱。并提出了相应的致死模型。最后得到了一个破片超高速撞击双板时的损伤概率。研究航天器的易损性分析和杀伤力数学模型,对增强我国的空间防御能力具有一定的参考意义和重要的现实意义。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Study on Vulnerability Model of Spacecraft Impacting by Orbital Debris
The spacecraft was studied. Spacecraft vulnerability was analyzed in some aspects as environment, representative structure, aviation theory, damage principle and existence speciality. Then the destruction types were advanced on debris against double plates. The damage types included local perforation and avulsion. And the respective lethality model was put forward. At last the damage probability was obtained when one fragment impacts the double boards by hypervelocity. It is a certain reference and important reality signification, that the vulnerability analysis and lethality mathematical model of spacecraft are researched, to strengthen our space defense ability.
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