Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile
Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile
- New search for: R. G. Norell
- New search for: R. G. Norell
The report documents the results of a study in which the aerodynamic stability and performance coefficients of the XSM-65A missile were determined for the range of flight conditions encountered during the powered flight phase of the missile trajectory. The study was undertaken to provide criteria for missile autopilot and roll control system design and data for use in trajectory performance computations. (AUTHOR)
Document information
Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile
1956
34 pages
Report
No indication
English
Missile Technology , Fluid Mechanics , Surface to surface missiles , Aerodynamic characteristics , Automatic pilots , Roll , Control systems , Guided missile trajectories , Drag , Stability , Pitch(Motion) , Wind tunnel models , Angle of attack , Center of gravity , Curve fitting , Atlas , Xsm-65a missiles
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