Attitude Motion and Aerodynamic Characteristics of MUSES-C Reentry Capsule
スポンサーリンク
概要
- 論文の詳細を見る
In order to realize the aerodynamic motion of the MUSES-C reentry capsule, several kinds of wind tunnel tests were conducted using the ISAS facilities. Adding to the ground test data, the aerodynamic properties in hypersonic flow were numerically analyzed
- 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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Ishii Nobuaki
Institute Of Space And Astronautical Science
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HIRAKI Koju
Kyushu Institute of Technology
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INATANI Yoshifumi
The Institute of Space and Astronautical Science, JAXA
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Hiraki Koju
Institute of Space and Astronautical Science (ISAS)
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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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