Set of curves presented from which stagnation-point equilibrium wall temperature during rocket-powered ascent, steady-state hypersonic flight, and re-entry, can be derived; most ballistic missile trajectories fall within range covered by these curves.
Figuring heating of blunt shapes in hypersonic flight
Space/Aeronautics
Space/Aeronautics ; 34 , n 4
1960
Aufsatz (Zeitschrift)
Englisch
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