Thermal Protection System of the Reentry Capsule with Superorbital Velocity
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概要
- 論文の詳細を見る
In the final phase of the MUSES-C mission, a small capsule with asteroid sample conducts reentry flight directly from the interplanetary transfer orbit at the velocity over 12 km/s. The severe heat flux, the complicated functional requirements, and small
- 宇宙航空研究開発機構の論文
著者
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Ishii Nobuaki
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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Ishii Nobuaki
The Institute Of Space And Astronautical Science Jaxa
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INATANI Yoshifumi
Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
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Yamada Tetsuya
Institute of Space and Astronautical Science (ISAS)
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Yamada Tetsuya
The Institute Of Space And Astronautical Science Jaxa
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Yamada Tetsuya
Institute Of Space And Astronautical Science
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Hinada Motoki
Ihi Aerospace Company
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Ishii Nobuaki
Institute Of Space And Astronautical Science
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INATANI Yoshifumi
The Institute of Space and Astronautical Science, JAXA
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Honda Masahisa
IHI Aerospace Company
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Inatani Y
The Institute Of Space And Astronautical Science Jaxa
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Inatani Yoshifumi
Institute Of Space And Astionautical Science Japan Aerospace Exploration Agency
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