Hypervelocity Impact Testing of a Metallic Glass-Stuffed Whipple Shield

被引：36

作者：

Hofmann, Douglas C. ^{[1
,2
]}

Hamill, Lee ^{[3
]}

Christiansen, Eric ^{[4
]}

Nutt, Steve ^{[3
]}

机构：

[1] CALTECH, Jet Prop Lab, Pasadena, CA 91125 USA

[2] CALTECH, Keck Lab Engn Sci, Pasadena, CA 91125 USA

[3] Univ So Calif, Los Angeles, CA USA

[4] NASA, Johnson Space Ctr, Houston, TX USA

来源：

ADVANCED ENGINEERING MATERIALS | 2015年 / 17卷 / 09期

关键词：

ORBITAL DEBRIS; HONEYCOMB;

D O I：

10.1002/adem.201400518

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

In this work, hypervelocity impact tests up to 7 km.s(-1) are used to compare the performance of Whipple shields integrated with layers of metallic glasses with a baseline target analogue of one of the shields similar to what is used on the International Space Station. The baseline target failed under the impact while the target utilizing metallic glass as a replacement for the fabric layers in the baseline passed the test. The paper postulates on the prospects of future implementation of metallic glasses as spacecraft debris shields.

引用

下载

页码：1313 / 1322

页数：10

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