FIELD: missile launchers.
SUBSTANCE: the method consists in the fact that a high-frequency impact load on the body of the high-pressure chamber and the powder charge is produced before the ignition of the powder charge. After the ignition the process of burning of the powder charge is accompanied with re-plenishment by high-temperature pyrotechnical gases with a warming-up and turbulizing action of them on the flow of gases elapsing from the high-pressure chamber. The high-pressure chamber in the recoilless gun is provided with a tapered prechamber n the rear nozzle unit accommodating the burning follower, and the electric primer in the central nipple. A damper cavity is formed under the electric primer, it is connected to the prechamber through a hole oriented to the bearing surface of the prechamber and the rear multi-nozzle grid. The throttle ports of the prechamber are oriented at an acute angle to the axis of the rear nozzles. The rear and front multi-nozzle grids are made with intersecting ducts for passage of gases in projection to each other.
EFFECT: enhanced muzzle velocity of the missile in the temperature range of combat employment.
2 cl, 4 dwg
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Authors
Dates
2007-02-27—Published
2005-07-01—Filed