FIELD: equipment of launching rocket systems.
SUBSTANCE: invention relates to rocket launchers, particularly, to carrier rocket launcher components cooling. To cool down the launcher at rocket launch, coolant is continuously fed into the jet flow zone of the propulsion system during its operation. Cooling fluid is supplied to the flue gas duct of the launching device by the piston pressure on the liquid located in the reservoir located inside the launching facility under the launching device. Pressure on piston is provided by gas jet from propulsion system.
EFFECT: cooling of launching device elements and provision of their long-term operation.
1 cl, 2 dwg
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