Tabulated pressure data are presented on the orbiter fuselage and left vertical tail surface of a scale model of the integrated space shuttle 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 3
1975
704 pages
Report
Keine Angabe
Englisch