Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90-degrees
EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG
1961-02-01
Report
No indication
English