Performance of Transpiration Cooled Heat Shields for Re-entry Vehicles - Dataset
This paper presents results of a system study of transpiration cooled thermal protection systems for Earth re-entry. The cooling performance for sustained hypersonic flight and transient re-entry of a blunt cone geometry is assessed. A simplified numerical model is used to calculate the transient te...
Main Authors: | Hermann, T, McGilvray, M, Naved, I |
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Formato: | Dataset |
Idioma: | English |
Publicado em: |
University of Oxford
2022
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