Aviation Glossary - Turbojet Engine

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Turbojet Engine

A jet engine incorporating a turbine-driven air compressor to take in and compress air for the combustion of fuel, the gases of combustion being used both to rotate the turbine and create a thrust producing jet.

source: FAA Airplane Flying Handbook (FAA-H-8083-3A)

A gas turbine engine that produces thrust by accelerating the air flowing through it. A minimum of energy is extracted by the turbine, with the majority used to produce an exhaust velocity much greater than the inlet velocity. The amount of thrust produced by the engine is determined by the amount the air is accelerated as it flows through the engine.

source: FAA Aviation Maintenance Technician Powerplant Handbook (FAA-H-8083-32)

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