Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1990-08-14
1991-08-20
Carone, Michael J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 33, F42B 1018
Patent
active
050407465
ABSTRACT:
A finned projectile intended to be launched toward a target has a project body and a plurality of main fins attached to the projectile body to provide stability thereto in flight. In the preferred embodiment, each main fin includes a supplementary fin movably secured thereto for increasing the overall surface area to further enhance the stability of the projectile after launch. A pin and channel arrangement is used for slidably retaining the supplemental fin and the main fins together for deployment under forces on the projectile during launch and flight thereof. The channel arrangement further includes a portion which angles suddenly to lock the supplementary fin in the deployed position. The preferred embodiment also includes putty disposed within the channel for preventing deployment of the supplementary fin during normal handling of the projectile. The putty is shattered upon initial impact with the pin during launching of the projectile.
REFERENCES:
patent: 1276892 (1918-08-01), Fender
patent: 3165281 (1965-01-01), Gohlke
patent: 3304030 (1967-02-01), Weimholt et al.
patent: 3633846 (1972-01-01), Biggs
patent: 4209146 (1980-01-01), Mattson
patent: 4440360 (1984-04-01), Hallstrom
patent: 4641802 (1987-02-01), Zalmon et al.
patent: 4667899 (1987-05-01), Wedertz
Baylor Walter R.
Carone Michael J.
Elbaum Saul
The United States of America as represented by the Secretary of
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