Self-cocking rocket launcher detent

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

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Details

89 1814, F41F 304

Patent

active

039584909

ABSTRACT:
A prior art rocket detent mechanism is provided with a lever operated cable ull attached to the rotatable detent such that the rocket tube may be reloaded and the detent reset without the necessity of reaching into the launcher tube with special tools. The lever is integral with the forward end of the reset rod and a cable affixed thereto is threaded through a pair of pad eyes and attached to the rotary detent pawl. Rotation of the rod and lever with respect to the forward pad eye exerts sufficient tension on the cable to reposition the detent when reloading the launcher tube.

REFERENCES:
patent: 2751818 (1956-06-01), Bonnett
patent: 2764066 (1956-09-01), Doak et al.
patent: 2830496 (1958-04-01), Anderson et al.
patent: 2830497 (1958-04-01), Smoot et al.
patent: 2938431 (1960-05-01), Dixon
patent: 3842711 (1974-10-01), Bodinaux

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