Tabulated force data and plotted pressure data are presented on a scale model of the integrated space shuttle vehicle configuration.
Results of a Pressure Loads Investigation on a 0.030-Scale Model (451-Ots) of the Integrated Space Shuttle Vehicle Configuration 5 in the NASA Ames Research Center 11 by 11 Foot Leg of the Unitary Plan Wind Tunnel (Ia81a), Volume 2
1975
817 pages
Report
Keine Angabe
Englisch