Review on hypervelocity impact of advanced space debris protection shields

被引:0
|
作者
Chen, Ying [1 ,2 ]
Tang, Qun-yi [1 ,2 ]
He, Qi-guang [3 ]
Chen, Lv-tan [1 ,2 ]
Chen, Xiao-wei [1 ,4 ]
机构
[1] Beijing Inst Technol, State Key Lab Explos Sci & Technol, Beijing 100081, Peoples R China
[2] Beijing Inst Technol, Sch Mechatron Engn, Beijing 100081, Peoples R China
[3] China Acad Engn Phys, Inst Fluid Phys, Lab Shock Wave & Detonat Phys, Mianyang 621900, Sichuan, Peoples R China
[4] Beijing Inst Technol, Adv Res Inst Multidisciplinary Sci, Beijing 100081, Peoples R China
基金
中国国家自然科学基金;
关键词
Advanced space debris protection shields; Hypervelocity impact; Debris cloud model; Numerical method; Phase transition; SMOOTHED PARTICLE HYDRODYNAMICS; CELL ALUMINUM FOAM; HONEYCOMB SANDWICH PANELS; PLATE LAUNCH CAPABILITY; MATERIAL POINT METHOD; NUMERICAL-SIMULATION; WHIPPLE SHIELD; COMPOSITE-MATERIALS; BALLISTIC LIMIT; ELEMENT-METHOD;
D O I
10.1016/j.tws.2024.111874
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Spacecraft employ space debris protection shields to mitigate the threat of hypervelocity impact (HVI) from millimeter-sized (envisioned in centimeters) hazardous space debris. Advancements in protection shields have primarily leveraged high-performance materials, such as high-performance fiber composites, multifunctional impedance gradient materials, and metallic honeycombs and foams, to enhance their protective capabilities. This paper provides a comprehensive overview of advanced space debris protection shields for HVI, covering the design and optimization of protective materials or structures, properties of debris clouds, phase transition issues of debris clouds, and numerical simulation techniques. Finally, to address the current research deficiencies considering the latest practical developments in space debris protection engineering, it is essential to propose engineering science research. These are important for enhancing the safety, stability, and longevity of spacecraft.
引用
收藏
页数:25
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