System and method for quenching a firing condition

Details System and method for quenching a firing condition System and method for quenching a firing condition

1992-04-28

1993-03-30

Brown, David H.

Ordnance

Rocket launching

Having safety devices for preventing premature ignition or...

89 181, 89 1816, F41F 304

Patent

active

051986108

ABSTRACT:
A system and method for suppressing heat around a missile housed in a canister during a restrained firing condition is provided. A missile canister has a hollow wall and an inner side provided with a plurality of dispensing holes. A coolant reservoir communicates with the canister wall via a coolant intake port. When a restrained firing condition occurs, gas is generated below the missile while the missile is physically restrained within the canister. The gas pressure impinges on a flexible face of the coolant reservoir causing its volume to decrease and coolant to be urged into the canister wall and out of the dispensing holes.

REFERENCES:
patent: 1264390 (1918-05-01), Hamilton
patent: 2560269 (1951-07-01), Berner
patent: 3052303 (1962-09-01), Lapp
patent: 3183904 (1965-05-01), Barakauskas
patent: 3298278 (1967-01-01), Barakauskas
patent: 3320742 (1967-05-01), Troax
patent: 3703930 (1972-11-01), Lofstrand et al.
patent: 4397215 (1983-08-01), Stroud
patent: 4436016 (1984-03-01), Olmsted et al.

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