Projectile Hypervelocity Impact Simulation
スポンサーリンク
概要
- 論文の詳細を見る
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.
- 宇宙航空研究開発機構の論文
著者
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SAWAOKA Akira
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Techn
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Sawaoka A
Tokyo Inst. Technol. Yokohama Jpn
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Tamura Hideki
Department Of Anesthesia Hiroshima Red Cross & Atomic Bomb Survivors Hospital
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Sawaoka Akira
Center For Ceramics Research Research Laboratory Of Engineering Materials Tokyo Institute Of Technol
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TAMURA Hideki
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Techn
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UEDA Keiji
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Techn
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USUI Toshichika
Center for Ceramics Research, Research Laboratory of Engineering Materials, Tokyo Institute of Techn
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Usui Toshichika
Center For Ceramics Research Research Laboratory Of Engineering Materials Tokyo Institute Of Technol
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Ueda Keiji
Center For Ceramics Research Research Laboratory Of Engineering Materials Tokyo Institute Of Technol
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Tamura Hideki
Center For Ceramics Research Research Laboratory Of Engineering Materials Tokyo Institute Of Technol
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