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Ablative heatshield materials are traditionally characterized in extensive, resource-consuming experimental campaigns. We develop a simplified way to estimate some bulk material properties for conceptual design and manufacturing evaluations.
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This page is a summary of: Constitutive Model of Fiber Substrate Ablators for Conceptual Design, Journal of Spacecraft and Rockets, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34371.
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