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Renewed interest in Mars exploration triggered the development of new missions. The radiative heat flux received by the backshell of the spacecraft during its atmospheric entry being dominant, we performed experiments and developed a numerical model able to simulate the nonequilibrium radiation.

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This page is a summary of: Simulations of CO2-CO Infrared Radiation Measurements in Shock and Expansion Tubes, Journal of Thermophysics and Heat Transfer, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t5853.
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