Gas generator missile launch system

Ordnance – Recoilless gun – Having pressure-control means

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89 1704, F41A 108

Patent

active

049626892

ABSTRACT:
A missile launching system with an open-ended cylindrical container (10) having a bore in which a slidable piston (20) is located between the missile (12) and a gas generator (14) adjacent the container aft end (16). The piston (20) area is substantially the same as the container bore at the aft end (16). An internal ring (42) forms a reduced area throat for gas exiting via the aft end of the container (10) with the ratio of the piston area to the throat area, A.sub.p /A.sub.t, being functionally related to the propellant physical characteristics.

REFERENCES:
patent: 2949061 (1960-08-01), Benditt et al.
patent: 2987965 (1961-06-01), Musser
patent: 3035494 (1962-05-01), Musser
patent: 3129636 (1964-04-01), Strickland et al.
patent: 3215041 (1965-11-01), Dietsch et al.
patent: 3376764 (1968-04-01), Abramson
patent: 3380340 (1968-04-01), Bergman et al.
patent: 3490330 (1970-01-01), Walther
patent: 3610093 (1971-10-01), Mebus
patent: 3653288 (1972-04-01), Stauff et al.

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