Guided projectile

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

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Details

102/5

F42B 10/60 (2006.01) F41G 7/00 (2006.01) F42B 10/66 (2006.01) F42B 15/01 (2006.01)

Patent

CA 1320389

ABSTRACT OF THE DISCLOSURE A guided projectile, especially a propelled or ballistic missile, has its trajectory corrected by gas jets from pulse thruster disposed in at least one axial plane of the missile symmetrically on opposite sides of the center of gravity thereof and whose thrusts are countered, when no longer needed, by the operation of diametrically opposite pulse thrusters in the same plane and at the same side of the center of gravity. The pulse thrusters are formed as gas generators which can be triggered to feed respective nozzles. The projectile is also roll stabilized, e.g. by a rotatable empennage. The transverse thrusts produced by the pulse thrusters are controlled by a sensor which responds to deviations from the correct orientation of the missile. The invention is particularly applicable to self-guided or homing tactical weapons.

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