Experimental aerodynamic investigations have been made on a .0035 scale model North American RockwellGeneral Dynamics version of the space shuttle. Static stability and control data were obtained on the delta wing booster alone (B-20) and with the delta wing orbiter (134D) mounted in various positions on the booster. Six component aerodynamic force and moment data were recorded over an angle of attack range from -10 deg to 24 deg at 0 deg and 6 deg sideslip angles and from -10 deg to +10 deg sideslip at 0 deg angle of attack. Mach number ranged from 0.6 to 4.96. (Author)
Space Shuttle Static Stability and Control Investigation of Nr/Gd delta Wing Booster (B-20) AND DELTA Wing Orbiter (134D), Volume 1
1972
323 pages
Report
Keine Angabe
Englisch