Tabulated pressure data are presented on the right upper wing surface, right lower wing surface, and SRM booster of the integrated space shuttle vehicle configuration.
Results of a Pressure Loads Investigation on a 0.030-Scale Model (47-Ots) of the Integrated Space Shuttle Vehicle Configuration 5 in the NASA Ames Research Center 11 X 11 Foot Leg of the Unitary Plan Wind Tunnel (Ia81a), Volume 6
1975
775 pages
Report
Keine Angabe
Englisch