FIELD: rocketry and space engineering; transportation system designed for start, hoist, acceleration and placing in orbit payload from surface of atmosphere planet. SUBSTANCE: transportation system includes 1st stage of rocket with exit nozzle 4 of cruise engine and thrust ejector amplifier 5 mounted on it, upper stages 2 and payload 3. Ejector amplifier 5 may be made in the form of axisymmetrical confuser 6, cylindrical housing 7 and diffuser 8. Nozzle 4 may be mounted in bearings 10 for rotation about engine axis. Ball mouth 9 of nozzle 4 is provided with inclined corrugations for rotation and twisting active flow. Length of ejector amplifier is equal to 2-3 diameters of housing 7. EFFECT: increased degree of thrust amplification and enhanced economical efficiency of placing payload into orbit due to more effective process of interaction of active and passive flows. 3 cl, 6 dwg
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