FIELD: space engineering. SUBSTANCE: method includes flight of launch vehicle to area of launch of subsequent stages of transport system, launch and independent flight of these stages over injection trajectory. Injection of payload is effected at moment when atmospheric jet stream is present in area of launch of subsequent stages. Launch vehicle is brought into atmospheric jet stream and launch of subsequent stages of transportation system is effected in jet stream during flight in direction when jet stream increases ground speed of transportation system. launch of subsequent stages of transportation system with launch vehicle is effected in circumpolar jet stream at geographical latitude of 20 to 50 deg and altitude of 5000 to 20000 m. EFFECT: enhanced reliability. 4 cl
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