A Study of Thermal Protection System for HTV-R Reentry
スポンサーリンク
概要
- 論文の詳細を見る
HTV-R aims to return payloads from the ISS to the Earth in the near future mission. This system contains new technologies for reentry, especially a thermal protection system with low-density ablator. This paper describes technical issues and basic research of the thermal protection system for HTV-R to realize Japanese return missions from the ISS.
- 特定非営利活動法人 日本ロケット協会の論文
著者
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MIZUNO Masahito
Japan Aerospace Exploration Agency, Institute of Space Technology and Aeronautics
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Fujita Kazuhisa
Japan Aerospace Exploration Agency
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WATANABE Yasuhide
Japan Aerospace Exploration Agency
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Suzuki Toshiyuki
Japan Aerospace Exploration Agency
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OGASAWARA Toshio
Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science
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FUJII Keisuke
Japan Aerospace Exploration Agency, Chofu
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AOKI Takuya
Japan Aerospace Exploration Agency, Chofu
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ISHIDA Yuichi
Japan Aerospace Exploration Agency, Chofu
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FUJITA Kazuhisa
Japan Aerospace Exploration Agency, Chofu
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YAMADA Tetsuya
Japan Aerospace Exploration Agency, Sagamihara
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