AI-450 Turboshaft


Designed for the use on light helicopters and aircraft in the take-off weight class of 1500-4000 kg. Usable as part of aircraft twin-engine and single-engine power plants.

Takeoff (H=0 m; M=0; ISA +15ºC)
Power, hp 465
Specific fuel consumption, kg/h/hp 0.260
Air flow, kg/sec 1.72
Мax cruise (H=0 m; M=0; ISА +15ºC)
Sower, hp 300
Specific fuel consumption, kg/h/hp 0.297
Dimensions, mm 1,085 х 536 х 515
Weight, dry (without propfan), kg 103
Specified service life, h 3,000

Applicability

  • Ка-226

    Ка-226


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