Spoiler torque controlled supersonic missile

Details Spoiler torque controlled supersonic missile Spoiler torque controlled supersonic missile

F - Mech Eng,Light,Heat,Weapons

41

G

244/1.5

F41G 7/00 (2006.01) F42B 10/62 (2006.01) F42B 15/00 (2006.01)

Patent

CA 2031283

A supersonic guided missile has a fuselage terminating at the front in a nose and at the rear in a base and is provided externally with fixed rear planes. At a longitudinal distance from the center of gravity is at least one spoiler mobile transversely between a configuration retracted inside the fuselage and an active configuration in which the spoiler projects laterally from the fuselage.

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