Missile appendage deployment mechanism

Details Missile appendage deployment mechanism Missile appendage deployment mechanism

1984-10-11

1987-05-12

Kyle, Deborah L.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

244 329, F42B 1332

Patent

active

046643397

ABSTRACT:
A missile appendage deployment mechanism for receipt on the side of a missile or projectile and in a stowed position. The mechanism including a wing or fin which is designed, when deployed, to rotate upwardly from the stowed position into a feathered vertical position into the airstream of the missile. The wing moves upwardly from the horizontal stowed position into the vertical feathered position in a continuous smooth motion.

REFERENCES:
patent: 3063375 (1962-11-01), Hawley et al.
patent: 3098445 (1963-07-01), Jackson
patent: 3127838 (1964-04-01), Moratti et al.
patent: 3185097 (1965-05-01), Cushing et al.
patent: 3695556 (1972-10-01), Gauzza et al.
patent: 4209146 (1980-06-01), Mattson
patent: 4323208 (1982-04-01), Ball

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