Research and development on hypervelocity impact protection using Whipple shield: An overview

被引:48
|
作者
Wen, Ken [1 ,2 ]
Chen, Xiao-wei [1 ]
Lu, Yong-gang [2 ]
机构
[1] Beijing Inst Technol, State Key Lab Explos Sci & Technol, Beijing 100081, Peoples R China
[2] China Acad Engn Phys, Inst Syst Engn, Mianyang 621999, Sichuan, Peoples R China
来源
DEFENCE TECHNOLOGY | 2021年 / 17卷 / 06期
基金
中国国家自然科学基金;
关键词
Space debris; Hypervelocity impact; Debris cloud; Whipple shield; Ballistic limit; SMOOTHED PARTICLE HYDRODYNAMICS; FINITE-ELEMENT-METHOD; THIN ALUMINUM SHEETS; HONEYCOMB SANDWICH PANEL; BALLISTIC LIMIT CURVES; DEBRIS CLOUD STRUCTURE; MATERIAL POINT METHOD; HOLE-DIAMETER; SPHERICAL PROJECTILES; NONSPHERICAL PROJECTILES;
D O I
10.1016/j.dt.2020.11.005
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Whipple shield, a dual-wall system, as well as its improved structures, is widely applied to defend the hypervelocity impact of space debris (projectile). This paper reviews the studies about the mechanism and process of protection against hypervelocity impacts using Whipple shield. Ground-based experiment and numerical simulation for hypervelocity impact and protection are introduced briefly. Three steps of the Whipple shield protection are discussed in order, including the interaction between the projectile and bumper, the movement and diffusion of the debris cloud, and the interaction between the debris cloud and rear plate. Potential improvements of the protection performance focusing on these three steps are presented. Representative works in the last decade are mentioned specifically. Some prospects and suggestions for future studies are put forward. (c) 2020 China Ordnance Society. Publishing services by Elsevier B.V. on behalf of KeAi Communications Co. Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
引用
收藏
页码:1864 / 1886
页数:23
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