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The proposed work will build on previous work supported under the R3 program and shift focus to the development of reliable gas-surface interaction models for Venus atmospheric entry. The model development will be specifically designed for Thermal Protection Systems made of woven carbon preform. The effect of the TPS structure with the high-pressure high-temperature effects of the atmosphere will be studied, including the effects of radiation penetration, due to the expected presence of CN gas in the post-shock region.
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