填充空心球/铝基复合材料结构的超高速撞击损伤特性研究

郑 伟;庞宝君;李 锋;陈 勇

振动与冲击 ›› 2013, Vol. 32 ›› Issue (18) : 141-145.

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振动与冲击 ›› 2013, Vol. 32 ›› Issue (18) : 141-145.
论文

填充空心球/铝基复合材料结构的超高速撞击损伤特性研究

  • 郑 伟1,庞宝君1,李 锋2,陈 勇1
作者信息 +

Research on damage characteristics of cenosphere/aluminum matrix composite stuffed shield under hypervelocity impact

  • ZHENG Wei1, PANG Bao-Jun1, LI Feng2, CHEN Yong1
Author information +
文章历史 +

摘要

针对人类航天活动在空间中积累的大量空间碎片严重威胁在轨运行航天器安全,急需开发具有优良防护性能的新材料防护结构问题,初步研究填充空心球/铝基复合材料Whipple防护结构的撞击特性,获得相关撞击损伤数据,与填充实心铝板的Whipple防护结构进行对比,并评估空心球/铝基复合材料作为一种航天器防护材料的可行性。

Abstract

Plenty of space debris has been produced by human action in space. It is constantly accumulating to pose a threat for the normal operation of the in-orbit spacecraft. So exploiting new material shielding structure with good performance will be one of major problems to explore for the national space debris protection field in the future. This paper has simply studied on impact property of cenosphere/aluminum matrix composite stuffed shield, then get some data related to impact damage, and be compared with solid aluminum stuffed shield. On this basis, the feasibility of cenosphere/aluminum matrix composite as a protective material for spacecraft has been evaluated.


关键词

空心球/铝基复合材料 / 空间碎片 / 超高速撞击 / 防护特性

Key words

cenosphere/aluminum matrix composite / space debris / hypervelocity impact / protective performance

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导出引用
郑 伟;庞宝君;李 锋;陈 勇. 填充空心球/铝基复合材料结构的超高速撞击损伤特性研究[J]. 振动与冲击, 2013, 32(18): 141-145
ZHENG Wei;PANG Bao-Jun;LI Feng;CHEN Yong. Research on damage characteristics of cenosphere/aluminum matrix composite stuffed shield under hypervelocity impact[J]. Journal of Vibration and Shock, 2013, 32(18): 141-145

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