Improved maneuverability and controllability are prime goals in meeting a broad spectrum of tactical missile requirements. Configuration based on the Vought 'Propulsion Augmented Control/Lift Surface' (PACS) approach to aeropropulsive integration are candidates for satisfying these requirements. The PACS concept utilizes a jet issuing from a trailing edge nozzle to induce augmented control loadings over fin or wing planforms. The current work provides experimental validation of PACS feasibility for a representative missile fin geometry at typical supersonic/transonic conditions. (Author)
Propulsion Augmented Control/Lift Surface Validation for Missile Maneuver Application
1982
158 pages
Report
No indication
English
Missile Guidance & Control Systems , Aerodynamics , Propulsion systems , Augmentation , High lift , Maneuverability , Aerodynamic stability , Guided missiles , Exhaust gases , Bleed systems , Trailing edges , Nozzles , Supersonic flow , Transonic flow , Airfoils , Injection , Flaps(Control surfaces) , Planform , Fins , Aerodynamic control surfaces , Angle of attack , Feasibility studies , Coefficients , Data bases
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