Turbopropmotor
A turbopropengine, or turbopropmotor, is an aircraft propulsion system in which a gas turbine generates power to drive a propeller through a reduction gearbox. Most of the energy from the turbine is converted into mechanical power to turn the propeller, producing thrust primarily by propulsion from the propeller rather than by jet exhaust alone. Some exhaust does contribute a small amount of jet thrust.
Principle of operation: Air is drawn in and compressed, then mixed with fuel and combusted. High‑temperature
Design and variants: A key feature is the reduction gearbox, which allows a high‑speed turbine to rotate
Performance and use: Turboprops are most efficient at medium altitudes and subsonic speeds, typically below about
History: Development began in the 1940s, with notable early designs such as the NK‑12 used on the