| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
Projectile Hypervelocity Impact Simulation |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| 著者 |
TAMURA, Hideki
UEDA, Keiji
USUI, Toshichika
SAWAOKA, Akira B.
|
| 著者所属（英） |
|
|
|
en |
|
|
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Technology |
| 著者所属（英） |
|
|
|
en |
|
|
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Technology |
| 著者所属（英） |
|
|
|
en |
|
|
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Technology |
| 著者所属（英） |
|
|
|
en |
|
|
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Technology |
| 出版者 |
|
|
出版者 |
宇宙科学研究所 |
| 出版者（英） |
|
|
出版者 |
Institute of Space and Astronautical Science |
| 書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Workshop on Space Debris May 11, 1989 at ISAS Conference Hall
巻 11,
p. 21-29,
発行日 1990-03
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
For the hypervelocity impact simulation of micrometeoroids on a space station, a plasma accelerator was constructed and tested to achieve projectile velocity of 10 km/s. Then the morphology of craters on an aluminum alloy target was investigated. The dual element shield structure consisting of aluminum alloy was tested up to 5 km/s impact. The morphology of impact area and the new technique of projectile emission was also reported. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0288-433X |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA10455137 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0033441000 |
SA0033441.pdf (900.5 kB)
