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Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact

Siyuan Ren Pinliang Zhang Qiang Wu Qingming Zhang Zizheng Gong Guangming Song Renrong Long Liangfei Gong Mingze Wu

Defence Technology(防务技术)2025，Vol.45Issue(3)：P.137-177,41.

Defence Technology(防务技术)2025，Vol.45Issue(3)：P.137-177,41.DOI:10.1016/j.dt.2024.09.002

Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact

Siyuan Ren ¹Pinliang Zhang ¹Qiang Wu ¹Qingming Zhang ²Zizheng Gong ¹Guangming Song ¹Renrong Long ²Liangfei Gong ³Mingze Wu²

作者信息

1. Beijing Institute of Spacecraft Environment Engineering,China Academy of Space Technology,Beijing,100094,China
2. State Key Laboratory of Explosion Science and Technology,Beijing Institute of Technology,Beijing,100081,China
3. School of Civil Engineering,Chongqing Jiaotong University,Chongqing,400074,China
折叠

摘要

关键词

Orbital debris/Spacecraft shield/Hypervelocity impact/Bumper materials/Protective mechanism

分类

航空航天

引用本文复制引用

Siyuan Ren,Pinliang Zhang,Qiang Wu,Qingming Zhang,Zizheng Gong,Guangming Song,Renrong Long,Liangfei Gong,Mingze Wu..Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact[J].Defence Technology(防务技术),2025,45(3):P.137-177,41.

基金项目

supported by National Natural Science Foundation of China(Grant Nos.12202068,12202087) （Grant Nos.12202068,12202087）

China National Space Administration Preliminary Research Project(Grant Nos.KJSP2023020201,KJSP2020010402). （Grant Nos.KJSP2023020201,KJSP2020010402）

Defence Technology(防务技术)

ISSN：2096-3459

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