Application of SWRC hypervelocity launcher to space debris bumper shield design

被引：0

作者：

Hashimoto, T ^{[1
]}

Takayama, K ^{[1
]}

Saito, T ^{[1
]}

Kobayashi, M ^{[1
]}

Kato, I ^{[1
]}

Togami, K ^{[1
]}

机构：

[1] Tohoku Univ, Inst Fluid Sci, Interdisciplinary Shock Wave Res Ctr, Sendai, Miyagi 9808577, Japan

来源：

SPACE DEBRIS AND SPACE TRAFFIC MANAGEMENT SYMPOSIUM 2003 | 2004年 / 109卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Paper reports results of two-stage light gas gun experiments of basic data acquisition for space debris bumper shield research performed at the Interdisciplinary Shock Wave Research Center (ISWRC) of Tohoku University. Primary hyper-velocity impact tests were carried out to visualize projectile impingements on bumpers made of aluminum at normal and oblique angles. Resulting debris clouds between normal and oblique impacts were compared. Numerical simulations conducted by AUTODYN-2D were validated by experiments of ultra high molecular weight polyethylene (UHMW-PE) projectile impacts against metallic bumpers.

引用

页码：309 / 318

页数：10

共 50 条

[1] Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact
Siyuan Ren
Pinliang Zhang
Qiang Wu
Qingming Zhang
Zizheng Gong
Guangming Song
Renrong Long
Liangfei Gong
Mingze Wu
Defence Technology, 2025, 45 (03) : 137 - 177
[2] Hypervelocity impacts on thin metallic and composite space debris bumper shields
Ramjaun, D
Kato, I
Takayama, K
Jagadeesh, G
AIAA JOURNAL, 2003, 41 (08) : 1564 - 1572
[3] Hypervelocity impacts on thin metallic and composite space debris bumper shields
Ramjaun, D., 1600, American Inst. Aeronautics and Astronautics Inc. (41):
[4] Evaluation of bumper shield with protuberants under space debris impact
Akahoshi, Y
Watanabe, D
Hata, H
SPACE DEVELOPMENT AND COOPERATION AMONG ALL PACIFIC BASIN COUNTRIES, 2002, 110 : 385 - 394
[5] Projectile shape effects for hypervelocity impact on space debris protection shield
Department of Aeronautics and Astronautics
Memoirs of the Graduate School of Engineering, Kyushu University, 2000, 60 (01): : 1 - 20
[6] Protection of Whipple shield against hypervelocity impact of space debris: a review
Singh, Pradeep Kumar
Kumar, Manoj
SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 2024, 49 (02):
[7] Protection of Whipple shield against hypervelocity impact of space debris: a review
Pradeep Kumar Singh
Manoj Kumar
Sādhanā, 49
[8] Status of development of space-debris hypervelocity explosive multi-stage launcher
Geille, A.
International Journal of Impact Engineering, 1997, 20 (1 -5 pt 1) : 271 - 279
[9] A HYPERVELOCITY LAUNCHER FOR SIMULATED LARGE FRAGMENT SPACE DEBRIS IMPACTS AT 10 KM/S
TULLOS, RJ
GRAY, WM
MULLIN, SA
COURPALAIS, BG
AIAA/ASME/ASCE/AHS/ASC 30TH STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE, PTS 1-4: A COLLECTION OF TECHNICAL PAPERS, 1989, : 1623 - 1628
[10] Status of development of space-debris hypervelocity explosive multi-stage launcher
Geille, A
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1997, 20 (1-5) : 271 - 279

← 1 2 3 4 5 →