Noise controllable nozzle closure

Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake

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Details

23926515, 102 493, F02K 100, F02K 126

Patent

active

040331210

ABSTRACT:
A rocket motor nozzle closure for controlling the initial release of prese from the rocket motor nozzle to reduce the occurrence of high pressure shock fronts which are detrimental to the weapon operator. The mass and geometry of the nozzle closure are predetermined to fit the desired motor performance. The release of motor pressure is controlled by the rate of change of momentum of the nozzle closure.

REFERENCES:
patent: 3121310 (1964-02-01), Rice
patent: 3170288 (1965-02-01), Penza et al.
patent: 3228334 (1966-01-01), Oss
patent: 3910191 (1975-10-01), Williams

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