Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
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概要
- 論文の詳細を見る
This paper summarizes thermal responses of ablator for reentry capsules with superorbital velocity together with analysis method and the experimental data acquisition in the designing and development process of the MUSES-C reentry capsule. On the predicti
- 宇宙航空研究開発機構の論文
著者
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INATANI Yoshifumi
Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
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Hirai Ken'ichi
Ihi Aerospace Company
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Yamada Tetsuya
Institute of Space and Astronautical Science (ISAS)
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Yamada Tetsuya
Institute Of Space And Astronautical Science
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Inatani Yoshifumi
Institute Of Space And Astionautical Science Japan Aerospace Exploration Agency
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