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The study of 5A06 aluminum alloy and aluminum matrix composite sheet behaviors of hypervelocity impact

  • Wei Ding*
  • , Gao Xiang Wu
  • , Xiu Hua Sun
  • , Zi Yang Xiu
  • , Dong Hua Zhang
  • , Long Tao Jiang
  • , Gao Hui Wu
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Qiqihar North Machinery Corporation Limited
  • China Aerospace Science and Technology Corporation
  • Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

With more frequent space launch activities, the rapid increase in the number of space debris on future space vehicles pose a threat to security. In order to research the materials of space debris, Tif/Al composite, Tif/Cf/Al composite and Cf/Al composite were fabricated by pressure infiltration technique. These materials were impacted by aluminum projectiles of different diameters from 0.8mm~2.0mm at the speed of 2.5 km/s. It can be judged from the critical diameter of the projectile staving in the material that Tif/Al composite is the best, and then the results of 5A06 aluminum alloy, Tif/Cf/Al composite materials, Cf/Al composite dropped. Measure and compare the various materials between the projectile diameter and pit depth discovery, Cf/Al composite materials, Tif/Cf/Al composite materials, Tif/Al composite materials, 5A06 aluminum projectile diameter and pit depth ratio reduced in turn.

Original languageEnglish
Pages (from-to)231-235
Number of pages5
JournalCailiao Kexue yu Gongyi/Material Science and Technology
Volume19
Issue numberSUPPL. 1
StatePublished - Dec 2011

Keywords

  • Cf/Al composite
  • Hypervelocity impact
  • Tif/Al composite
  • Tif/Cf/Al composite

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