Development of a Radiation Analysis Code for Hypervelocity Reentry Applications

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概要

• 論文の詳細を見る

• The computer code SPRADIAN, a structured package for radiation analysis, has been developed. This study is primarily motivated by the MUSES-C sample return mission which encounters severe radiative environments during reentry into the earth atmosphere. In

• 宇宙航空研究開発機構の論文

著者

• Abe Takashi

  Institute of Space and Astronautical Science (ISAS)

• Fujita Kazuhisa

  Institute Of Space And Astronautical Science

• 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

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