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...

תיאור מלא

מידע ביבליוגרפי
Main Authors: Hermann, T, McGilvray, M, Naved, I
פורמט: Dataset
שפה:English
יצא לאור: University of Oxford 2022