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Damage characteristics of a cenosphere/aluminum matrix composite stuffed shield under hypervelocity impact

  • Wei Zheng*
  • , Bao Jun Pang
  • , Feng Li
  • , Yong Chen
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology
  • China Aviation Industry Corporation

Research output: Contribution to journalArticlepeer-review

Abstract

Plenty of space debris are produced by human in space. They are a threat to the normal operation of in-orbit spacecrafts. So, it is necessary to develop a new material shielding structure with a good protection performance. Here, the impact properties of a cenosphere/aluminum matrix composite stuffed shield were investigated. Then, some data related to impact damage were obtained, and they were compared with those of a whipple protection structure using solid aluminum stuffed shield. On this basis, the feasibility of cenosphere/aluminum matrix composite material as a protection material for spacecraft was evaluated.

Original languageEnglish
Pages (from-to)141-145
Number of pages5
JournalZhendong yu Chongji/Journal of Vibration and Shock
Volume32
Issue number18
StatePublished - 28 Sep 2013
Externally publishedYes

Keywords

  • Cenosphere/aluminum matrix composite
  • Hypervelocity impact
  • Protection performance
  • Space debris

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