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250-C30U

250-C30U is a turboshaft engine model used in aircraft.

Specifications

Engine Family: turboshaft

Compressor stages: 1

Control system: EECU

Dry weight: 115 kilogram

Gas generator stages: 2

Height: 0.64 metre

Length: 1.1 metre

Max. continuous power: 447 kilowatt

Max. takeoff power: 485 kilowatt

Ng RPM: 51000

Output shaft RPM: 6016

Power turbine stages: 2

Width: 0.56 metre

Manufacturer

Rolls-Royce