航天器可防护/感知一体化结构技术方案  

The Technical Scheme of Integrated Structure for Shielding and Perception for Spacecraft

作　　者：徐欣 邓卫华 龚自正[2] 张品亮 刘江 XU Xin;DENG Wei-hua;GONG Zi-zheng;ZHANG Pin-liang;LIU Jiang(DFH Satellite Co.,Ltd,China Academy of Space Technology,Beijing 100094,China;Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China)

机构地区：[1]中国空间技术研究院航天东方红卫星有限公司,北京100094 [2]中国空间技术研究院总装与环境工程部,北京100094

出　　处：《空间碎片研究》2022年第2期11-17,共7页Space Debris Research

摘　　要：目前,我国除了空间站外,其他航天器均未进行空间碎片防护设计,处在空间碎片超高速撞击的严重威胁之下。在我国现有的高强度先进防护材料的研究基础上,以航天器的可防护/感知一体化结构设计为目标,探究将空间碎片防护、隔热和撞击感知等多种功能集成于航天器结构中,构建航天器一体化结构的综合性能评价方法与体系。Except for the space station, China’s spacecraft have not been designed for space debris shielding, and thus being faced with the serious threat of hypervelocity impact of space debris.Based on the existing high strength advanced shielding materials in China and aiming at the integrated structure of shielding and perception for spacecraft, we have been exploring the integration of the space debris shielding, insulation, perception and other functions into the spacecraft structure, establishing comprehensive evaluation method for integrated structure of spacecraft.

关 键 词：空间碎片 航天器防护 

分 类 号：V528[航空宇航科学与技术—人机与环境工程]