Aerodynamic Damping and Oscillatory Stability in Pitch and Yaw of Gemini Configurations at Mach Numbers from 0.50 to 4.63
1966
73 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Aerodynamic characteristics , Damping in pitch , Damping in yaw , Gemini spacecraft , Oscillation , Abort , Aerodynamic , Characteristics , Configuration , Damping , Measurement , Pitch , Reentry , Spacecraft , Speed , Stability , Supersonic , Transonic , Tune , Wind , Yaw