Attempt made to define maximum re-entry performance required of lifting re-entry vehicle, within limits imposed by maximum re-entry velocity of 36,000 fps; corresponding thermal environments established provide basis for examination of various thermal protection system concepts; systems which are believed sufficiently promising to justify further development are shown.
Thermal protection of lifting re-entry vehicles
Aerospace Eng
Aerospace Engineering ; 22 , n 1
1963
17 pages
Aufsatz (Zeitschrift)
Englisch
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