Integrated thrust vector aerodynamic control surface

Details Integrated thrust vector aerodynamic control surface Integrated thrust vector aerodynamic control surface

F - Mech Eng,Light,Heat,Weapons

42

B

102/5

F42B 15/00 (2006.01) F42B 13/24 (1980.01) F42B 13/30 (1980.01)

Patent

CA 1078253

Abstract of the Disclosure A missile is disclosed on which constant burning thrust reaction motors are provided integral with the tail panels of the missile to enhance the effect thereof, parti- cularly during the boost phase of flight. The motors provide thrust along the chord of the tail panel and are moved about the axis of rotation of the tail panel by the servo motor associated therewith. The servo motors are activated by central missile control circuitry.

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