A Study on Aerodynamic Heating at Jovian Atmospheric Aerocapture. I.
スポンサーリンク
概要
- 論文の詳細を見る
The numerical simulations of drag and aerodynamic heating to the spacecraft during Jovian aerocapture have been conducted. DSMC method is used for the simulations of flow fields around the spacecraft. The transient changes of drag due to Jovian atmosphere and total heat loads to the spacecraft are obtained. The results show the estimated heat loads could be within allowable heat load when proper ablation heat shield technique is applied. Also, the results shows Jovian aerocapture could save total mass of spacecraft or could increase payload of spacecraft compared with retro-rocket blowing for space flight to Jupiter.
- 九州大学の論文
- 2004-03-26
著者
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YASAKA Tetsuo
Department of Aeronautics and Astronautics
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HIRAYAMA Hiroshi
Department of Neurosurgery, Gifu University School of Medicine
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Hirayama Hiroshi
Department Of Aeronautics And Astronautics
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HATTA Shinji
Department of Aeronautics and Astronautics
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ASO Shigeru
Department of Aeronautics and Astronautics
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Poetro Ridanto
Department of Aeronautics and Astronautics
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Aso S
Department Of Aeronautics And Astronautics
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