防务技术2024,Issue(1) :58-72.DOI:10.1016/j.dt.2023.01.009

Experimental and numerical study of hypervelocity impact damage on composite overwrapped pressure vessels

Yong-Pan Duan Run-Qiang Chi Bao-Jun Pang Yuan Cai
防务技术2024,Issue(1) :58-72.DOI:10.1016/j.dt.2023.01.009

Experimental and numerical study of hypervelocity impact damage on composite overwrapped pressure vessels

Yong-Pan Duan 1Run-Qiang Chi 1Bao-Jun Pang 1Yuan Cai2
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作者信息

  • 1. Hypervelocity Impact Research Center,Harbin Institute of Technology,Harbin,150080,China
  • 2. College of Science,Heilongjiang University of Science and Technology,Harbin 150022,China
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Abstract

Ground-based tests are important for studying hypervelocity impact(HVI)damage to spacecraft pressure vessels in the orbital debris environment.We analyzed the damage to composite overwrapped pressure vessels(COPVs)in the HVI tests and classified the damage into non-catastrophic damage and cata-strophic damage.We proposed a numerical simulation method to further study non-catastrophic damage and revealed the characteristics and mechanisms of non-catastrophic damage affected by impact conditions and internal pressures.The fragments of the catastrophically damaged COPVs were collected after the tests.The crack distribution and propagation process of the catastrophic ruptures of the COPVs were analyzed.Our findings contribute to understanding the damage characteristics and mechanisms of COPVs by HVIs.

Key words

Orbital debris/Hypervelocity impact/Composite overwrapped pressure vessels/Damage mechanisms

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基金项目

National Natural Science Foundation of China(11672097)

National Natural Science Foundation of China(11772113)

出版年

2024
防务技术
中国兵工学会

防务技术

CSTPCD
影响因子:0.358
ISSN:2214-9147
参考文献量23
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