Turbojet Engine

A type of gas turbine, or jet engine, that derives its thrust wholly from a rearward jet of hot gases. in a simple turbojet, air is taken in through the front of the engine and compressed by a compressor. The compressed air then feeds through nozzles into a combustion chamber, fuel is sprayed in, and the mixture is ignited. The hot gases produced expand through a turbine (which drives the compressor ) before escaping at high speed through a rear nozzle. reaction to the rearward jet produces a forward propulsive thrust. Practical turbojets hove two or more compressor and turbine stages.