Arrangement for the unlatching and extension of the stabilizing

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

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F42B 1020

Patent

active

051140950

ABSTRACT:
An arrangement for the unlatching and extension of the stabilizing fins or control surfaces of a projectile, including a power element which is effective in the longitudinal direction of the projectile for pressing a follower against camming or runoff edges located proximate hinged connections at the fin footings, after a latching for the stabilizing fin in the region of their end surfaces has been released. The power element causes a latching crown or ring to be raised away from the end surfaces of the stabilizing fins opposite the force of a spring through the longitudinal movement of a connecting or pusher rod prior to the pusher rod engaging behind the follower and then pressing against the runoff or camming edges.

REFERENCES:
patent: 2801587 (1957-08-01), Gould
patent: 4600167 (1986-07-01), Kastenhuber et al.
patent: 4659037 (1987-04-01), Unterstein
patent: 4860969 (1989-08-01), Muller et al.

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