Definition of entry corridor thermal limits for Apollo spacecraft.
Entry corridor thermal entry limits for Apollo spacecraft defined for design of thermal protection system
Curry, D. M.↗
Engineering topics
Posgay, R. G.
Publications and source records attributed to Posgay, R. G..
Thermo-structural failure limits for the spacecraft component for an Apollo 1B launch environment
Computer programs for analyzing aerodynamic heating effects on structural failure of Saturn 1 launch vehicle components
Faust, C. D.↗