FIELD: injection of payload into orbit by means of launch vehicle. SUBSTANCE: method consists in filling the launch vehicle with propellant in amount including the guaranteed reserve, flight of launch vehicle in injection trajectory, transfer of propellant from one stage to other and separation of payload. In filling the launch vehicle with propellant, guaranteed reserve of propellant is placed in next stage or in payload partially or fully; in-flight transfer of propellant is effected through delivery of guaranteed reserve of propellant to previous stage of launch vehicle. EFFECT: enhanced efficiency.
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