Apparatus for wing attachment

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

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Details

244 325, F42B 1006

Patent

active

050641425

ABSTRACT:
A saddle for restraining vibration of a wing of a missile. The saddle has a grooved portion adapted to receive the wing. The saddle has two legs extending away from the grooved portion which are secured to the missile.

REFERENCES:
patent: 2842058 (1958-07-01), Kuller et al.
patent: 3048109 (1962-08-01), Feemster
patent: 3117520 (1964-01-01), Kerr et al.
patent: 3228335 (1966-01-01), Thompson
patent: 3276377 (1966-10-01), Bell
patent: 3648953 (1972-03-01), Polk
patent: 4673146 (1987-06-01), Inglis

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