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Alan Viladegut Farran
Space re-entry is a challenging endeavor due to the harsh thermo-chemical environment around the vehicle. Heat flux being the reference parameter for Thermal Protection System (TPS) design, the total energy transfer can significantly increase due to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::456f87eff8b6be620e1da60a87da8079
https://doi.org/10.35294/phdt201804
https://doi.org/10.35294/phdt201804
