FIELD: rocketry.
SUBSTANCE: equipment for rocket launching systems, in particular a method for cooling elements of a launch vehicle discharger. To do this, when the launch vehicle is launched, the coolant constantly circulates through the heat removal channels in the metal lining of the launcher flue. The liquid is supplied simultaneously with the start of the propulsion system.
EFFECT: cooling of the elements of the starting device and ensuring their long-term operation.
1 cl, 2 dwg
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