FIELD: power engineering. SUBSTANCE: gas-turbine engine has turbocompressor, device for forced revolving of turbocompressor rotor 1, and combustion chamber 6 mounted for rotation relative to rotor 1 and carrying on its end nozzle assembly 7. Combustion chamber 6 is kinematically linked with device 9 for its forced rotation together with turbocompressor rotor 1. The latter and combustion chamber 6 are jointly forced in rotary motion at beginning of starting to feed air and fuel to combustion chamber 6 and to ignite air-fuel mixture. As soon as engine gains speed, turbocompressor rotor stops running. EFFECT: facilitated starting conditions. 5 cl, 4 dwg
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