An envelope portion of an airborne craft comprises a metallic outer wall and a metallic inner wall arranged interior to the outer wall. The outer and inner walls delimit an inter-wall volume configured to support a flow of coolant to cool the outer wall during atmospheric heating of the outer wall.
Active cooling of windward surface of craft
08.10.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIAA | 1976
|Tema Archiv | 1986
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