Measurement of mass, spray angle and velocity distribution of fragment cloud

被引:14
|
作者
Akahoshi, Y [1 ]
Kaji, M [1 ]
Hata, H [1 ]
机构
[1] Kyushu Inst Technol, Fac Engn, Dept Mech Engn, Tobata Ku, Kitakyushu, Fukuoka 8048550, Japan
关键词
space debris; flash X-ray; hypervelocity impact; two-stage light gas gun;
D O I
10.1016/j.ijimpeng.2003.10.029
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Space debris has monotonously increased since space development started all over the world. Although International Space Station (ISS) is under construction, we still have a problem of a collision with orbital debris, average relative impact velocity of which is 8.7 km/sec. Therefore the study of the bumper shields against space debris impacts is very important. A performance of the bumper shields depends on generating small fragments and scattering them widely to disperse their kinetic energy. The mass, the spray angle and the velocity distribution of the fragments are necessary to construct the kinetic energy distribution. The purpose of this study is construction of the mass, the spray angle, and the velocity distribution based on the state of the fragment cloud generated after the first bumper shield impact. The mass and the spray angle distribution were made by captured fragments, and the velocity distribution was constructed by making the three dimensional distribution of the fragment cloud using flash X-ray. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:845 / 853
页数:9
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