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The heating environment and material response experienced by the Galileo entry probe is investigated. We show, for the first time, a close prediction of heat shield recession due to careful selection of high fidelity modeling approaches.

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This page is a summary of: Investigation of Galileo Probe Entry Heating with Coupled Radiation and Ablation, Journal of Spacecraft and Rockets, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34751.
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