The working cycle of this type of engine is that of Brayton, it is similar to that of the reciprocal engine because it has the same disposition of the working times intake, compression, combustion and exhaust or expansion. A turbojet consists of an air inlet, an air compressor, a combustion chamber, a gas turbine which moves the air compressor and a nozzle. The air enters compressed in the chamber, is heated and expanded by the combustion of the fuel and then it is expelled through the turbine towards the nozzle being accelerated at high speeds to provide the propulsion

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