Missile control surface actuator system

Details Missile control surface actuator system Missile control surface actuator system

1983-09-26

1987-04-21

Tudor, Harold J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 327, F41G 700, F42B 1502

Patent

active

046590366

ABSTRACT:
An actuator system for use in positioning control surfaces on a missile in response to steering commands. The actuator system raising the control surfaces such as missile fins from a retracted position in the missile outwardly to the deployed position and rotating the fins for controlling and steering the missile.

REFERENCES:
patent: 2584127 (1952-02-01), Harcum et al.
patent: 3112902 (1963-12-01), Kongelbeck
patent: 3245352 (1966-04-01), Summers
patent: 3276332 (1966-10-01), Jaffe
patent: 3327592 (1967-06-01), Wilkinson
patent: 3415466 (1968-12-01), Poole, Jr.
patent: 3695556 (1972-10-01), Gauzza et al.
patent: 4052024 (1977-10-01), Smith
patent: 4085909 (1978-04-01), East et al.
patent: 4361073 (1982-11-01), Oelrich et al.

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