Spoiler torque controlled supersonic missile

Details Spoiler torque controlled supersonic missile Spoiler torque controlled supersonic missile

1990-12-12

1992-09-01

Carone, Michael J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 327, F42B 1062

Patent

active

051433206

ABSTRACT:
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.

REFERENCES:
patent: 2922600 (1960-01-01), Craft
patent: 3136250 (1964-06-01), Humphery
patent: 3188958 (1965-06-01), Burke et al.
patent: 3305194 (1967-02-01), Conard et al.
patent: 3588004 (1971-06-01), Suter
patent: 3759466 (1973-09-01), Evers-Euterneck
patent: 4327884 (1982-05-01), Lawhorn
patent: 4497460 (1985-02-01), Thorsted et al.
patent: 4699333 (1987-10-01), Pinson

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