FIELD: transport.
SUBSTANCE: invention relates to space engineering, namely, to spaceship launch complex. Proposed invention relates to launching multiunit rocket consisting of central unit and even number of lateral units and comprises isolating combustion products of separate units and deflecting vertical jets from lateral units in symmetry about combustion product jets from central unit in single horizontal direction. Jets from lateral units are deflected and turned so that, on leaving the flume, they run horizontally in one line with jets from central unit to form clearances between combustion product jets. Outer lateral surfaces of extreme jets are protected against spreading.
EFFECT: reduced acoustic and other harmful effects on rocket and launching equipment.
2 cl, 4 dwg
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