Experimental study of hypervelocity impact on multi-shock structure

Qing Ming Zhang; Yan Hai Chen; Feng Lei Huang

Experimental study of hypervelocity impact on multi-shock structure

Qing Ming Zhang^*, Yan Hai Chen, Feng Lei Huang

^*此作品的通讯作者

机电学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

Hypervelocity impact tests on multi-shock shields are carried out in order to develop space structures against space debris impacts. Sheets of LY12 aluminum were used as bumpers. The total thickness of shield structure, which consists of several sheets with various thickness, is 3.0 mm or 2.0 mm. The test results show that the type 0.5 mm + 0.5 mm + 0.5 mm + 0.5 mm is a better choice of spacecraft shield structure.

源语言	英语
页（从-至）	274-279
页数	6
期刊	Journal of Beijing Institute of Technology (English Edition)
卷	13
期	3
出版状态	已出版 - 9月 2004

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{e796b009ed54481fa6a7fc2328e6c934,

title = "Experimental study of hypervelocity impact on multi-shock structure",

abstract = "Hypervelocity impact tests on multi-shock shields are carried out in order to develop space structures against space debris impacts. Sheets of LY12 aluminum were used as bumpers. The total thickness of shield structure, which consists of several sheets with various thickness, is 3.0 mm or 2.0 mm. The test results show that the type 0.5 mm + 0.5 mm + 0.5 mm + 0.5 mm is a better choice of spacecraft shield structure.",

keywords = "Debris cloud, Hypervelocity, Multi-sheet structure, Space debris",

author = "Zhang, {Qing Ming} and Chen, {Yan Hai} and Huang, {Feng Lei}",

year = "2004",

month = sep,

language = "English",

volume = "13",

pages = "274--279",

journal = "Journal of Beijing Institute of Technology (English Edition)",

issn = "1004-0579",

publisher = "Beijing Institute of Technology",

number = "3",

}

TY - JOUR

T1 - Experimental study of hypervelocity impact on multi-shock structure

AU - Zhang, Qing Ming

AU - Chen, Yan Hai

AU - Huang, Feng Lei

PY - 2004/9

Y1 - 2004/9

N2 - Hypervelocity impact tests on multi-shock shields are carried out in order to develop space structures against space debris impacts. Sheets of LY12 aluminum were used as bumpers. The total thickness of shield structure, which consists of several sheets with various thickness, is 3.0 mm or 2.0 mm. The test results show that the type 0.5 mm + 0.5 mm + 0.5 mm + 0.5 mm is a better choice of spacecraft shield structure.

AB - Hypervelocity impact tests on multi-shock shields are carried out in order to develop space structures against space debris impacts. Sheets of LY12 aluminum were used as bumpers. The total thickness of shield structure, which consists of several sheets with various thickness, is 3.0 mm or 2.0 mm. The test results show that the type 0.5 mm + 0.5 mm + 0.5 mm + 0.5 mm is a better choice of spacecraft shield structure.

KW - Debris cloud

KW - Hypervelocity

KW - Multi-sheet structure

KW - Space debris

UR - http://www.scopus.com/inward/record.url?scp=9444297881&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:9444297881

SN - 1004-0579

VL - 13

SP - 274

EP - 279

JO - Journal of Beijing Institute of Technology (English Edition)

JF - Journal of Beijing Institute of Technology (English Edition)

IS - 3

ER -

Experimental study of hypervelocity impact on multi-shock structure

摘要

其它文件与链接

指纹

引用此