FIELD: rocketry. SUBSTANCE: electric current discharge is produced in area of reduced pressure, thus providing for supply of additional energy to propulsive mass and increasing pressure. Device is provided with pair of electrodes located in area of increased pressure after point of injection of propulsive mass which ensure supply of additional energy to propulsive mass at moment of electric discharge. EFFECT: compensation for reduction of cross-wind force at injection of propulsive mass into supersonic part of nozzle in area after injection hole. 2 dwg
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