Automatically deployed shell fins

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

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Details

F42B 1332

Patent

active

043323600

ABSTRACT:
A guided artillery shell is provided with a set of tail fins which are std within the shell assembly prior to the firing of the shell and during barrel traversal, and are automatically deployed upon muzzle exit by a mechanism responsive to the change in pressure upon muzzle exit and centrifugal force.

REFERENCES:
patent: 2821924 (1958-02-01), Hansen et al.
patent: 3289587 (1966-12-01), Donnelly et al.
patent: 3944168 (1976-03-01), Bizien et al.

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