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Transpiration Cooling can enhance the degree of reusability of spaceplanes and rockets. In this study, we experimentally examined the flow behaviour of porous Ultra-High-Temperature-Ceramics -- known for their high melting point (> 3000 K) -- for the purpose of transpiration cooling. The flow features demonstrate a good uniformity and thereby make them suitable candidates for this application.
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This page is a summary of: Flow Characterization of Porous Ultra-High-Temperature Ceramics for Transpiration Cooling, AIAA Journal, May 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061009.
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