改进的Whipple防护结构与相关数值模拟方法研究进展

Ying Chen, Xiaowei Chen*

*此作品的通讯作者

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10 引用 (Scopus)
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摘要

Based on the formation mechanism of the debris cloud caused by the projectile hypervelocity impacting onto a thin plate, the Whipple shield can effectively protect the spacecraft from space debris and micrometeoroid. By reviewing the research and development of the Whipple shield, and compares the mechanical effects and protective performance of multilayer, stuffed and sandwich shield. The paper also summarizes the application of numerical simulation methods and their improvement for the hypervelocity impact of protective structures containing materials such as foam and honeycomb, etc. By addressing the results of hypervelocity impact tests and numerical simulations of relevant materials, suggestions are made for the future research of the Whipple shield.

投稿的翻译标题A review on the improved Whipple shield and related numerical simulations
源语言繁体中文
文章编号021403
期刊Baozha Yu Chongji/Expolosion and Shock Waves
41
2
DOI
出版状态已出版 - 5 2月 2021

关键词

  • Debris cloud
  • FEM-SPH adaptive method
  • Hypervelocity impact
  • Multilayer shield
  • Stuffed/sandwich shield
  • Whipple shield

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引用此

Chen, Y., & Chen, X. (2021). 改进的Whipple防护结构与相关数值模拟方法研究进展. Baozha Yu Chongji/Expolosion and Shock Waves, 41(2), 文章 021403. https://doi.org/10.11883/bzycj-2020-0289