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...

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Bibliografische gegevens
Hoofdauteurs: Hermann, T, McGilvray, M, Naved, I
Formaat: Dataset
Taal:English
Gepubliceerd in: University of Oxford 2022