Yamada Tetsuya | Institute of Space and Astronautical Science (ISAS)
スポンサーリンク
概要
関連著者
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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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INATANI Yoshifumi
Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
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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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Yamada Tetsuya
The Institute Of Space And Astronautical Science Jaxa
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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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Nonaka Satoshi
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
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Nonaka Satoshi
Institute Of Space And Astionautical Science Japan Aerospace Exploration Agency
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OGAWA Hiroyuki
Institute of Molecular and Cellular Biosciences, The University of Tokyo
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Hirai Ken'ichi
Ihi Aerospace Company
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Nonaka Satoshi
Institute Of Space And Astronautical Science
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Nakakita Kazuyuki
National Aerospace Laboratory
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Yamazaki Takashi
National Aerospace Laboratory
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HIRAKI Koju
Kyushu Institute of Technology
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Hiraki Koju
Institute of Space and Astronautical Science (ISAS)
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Nakakita K
National Aerospace Laboratory
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Inatani Yoshifumi
Institute Of Space And Astronautical Science (isas)
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Ogawa Hiroyuki
Institute Of Space And Astronautical Science
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Ogawa Hiroyuki
Institute Of Molecular And Cellular Biosciences The University Of Tokyo
著作論文
- Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
- An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
- System Description and Reentry Operation Scenario of MUSES-C Reentry Capsule
- Thermal Protection System of the Reentry Capsule with Superorbital Velocity
- Arc Heating Facility and Test Technique for Planetary Entry Missions