Oveview of Research for Prediction of Aerodynamic Heating Environment during a Super-Orbital Reentry Flight of MUSES-C Reentry Capsule
スポンサーリンク
概要
著者
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Abe T
Institute Of Space And Astronautical Science
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Abe Takashi
Institute of Space and Astronautical Science (ISAS)
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Abe Takashi
Institute Of Space And Astronautical Science
関連論文
- Assessment of Forebody and Backbody Radiative Heating Rate of Hypervelocity Reentry Capsule
- Influences of Transport Model on Heating Rate of Reentry Vehicles
- Chemical Nonequilibrium Viscous Shock-Layer Analysis over Ablating Surface of Superorbital Re-Entry Capsule
- Oveview of Research for Prediction of Aerodynamic Heating Environment during a Super-Orbital Reentry Flight of MUSES-C Reentry Capsule
- Effect of the Flow Non-uniformity on the Mixing Layer at the Interface of Parallel Supersonic Flows
- Experimental Study of Nonequilibrium Phenomena behind Strong Shock Waves Generated in Super-orbital Reentry Flight
- Utilization of Expansion Tube for MUSES-C Reentry Simulation
- Study for Dynamically Unstable Motion of Reentry Capsule
- Development of a Radiation Analysis Code for Hypervelocity Reentry Applications
- Rarefied Aerodynamics of MUSES-C Sample Return Capsule