Missile detent and release apparatus

Ordnance – Rocket launching – Having means restraining rocket from movement in launching...

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Details

89 1812, F41F 304

Patent

active

057447454

ABSTRACT:
A missile detent and release apparatus which is capable of detaining and rapidly releasing a missile in a launch tube when conveying/launching the same, and in particular to an improved missile detent and release apparatus by which the missile is easily detained and rapidly released with only a small amount of force, and by which the missile can be stably detained in the launch tube conveying the missile, which includes a pair of detaining protrusions protruded from one end portion of a missile, a pair of fixing members fixed on an inner surface of a missile launch tube and having a detaining groove into which the detaining protrusion is inserted, with the fixing members being formed in the forwarding direction of the missile, a detaining screw passing through a detaining groove of each fixing member in the forwarding direction of the missile and engaged to a detaining screw hole formed at the center portion of the detaining protrusion for detaining the missile in the forwarding direction of the missile, a releasing rotation member rotatably engaged to the fixing member, and extending in the direction of the center of a missile nozzle, with the releasing rotation member being backwardly moved by a rocketing force of the missile, and a detaining pin for detaining the movement of the detaining screw, with the end portion thereof being fixed to the rotation member.

REFERENCES:
patent: 2879677 (1959-01-01), Herrmann
patent: 3296929 (1967-01-01), Jacobson
patent: 3398639 (1968-08-01), Apotheloz
patent: 3825980 (1974-07-01), Moore
patent: 4453449 (1984-06-01), Hollmann
patent: 4550640 (1985-11-01), Harter
patent: 5056407 (1991-10-01), Mathey

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