Assessment of Forebody and Backbody Radiative Heating Rate of Hypervelocity Reentry Capsule
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概要
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The thermally and chemically nonequilibrium hypersonic flow around the MUSES-C reentry capsule was analyzed to evaluate the radiative heating environment. The typical reentry speed is 11.6 km/s at the altitude of 64 km. Since the radiative heating strongl
- 宇宙航空研究開発機構の論文
著者
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Otsu Hirotaka
Shizuoka University
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Fujita K
Kyoto Univ. Kyoto Jpn
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Abe T
Institute Of Space And Astronautical Science
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Suzuki Kojiro
University of Tokyo
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Fujita Kazuhisa
Institute of Space and Astronautical Science (ISAS)
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Abe Takashi
Institute of Space and Astronautical Science (ISAS)
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Suzuki Kojiro
Department of Advanced Energy, Graduate School of Frontier Sciences, The University of Tokyo
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Suzuki K
Department Of Advanced Energy Graduate School Of Frontier Sciences The University Of Tokyo
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Fujita Kazuhisa
Institute Of Space And Astronautical Science
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Abe Takashi
Institute Of Space And Astronautical Science
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