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 )
Power, hp 465
Specific fuel consumption, kg/h/hp 0.260
Air flow, kg/sec 1.72
Мax cruise
Рower, hp 300
Specific fuel consumption, kg/h/hp 0.297
Weight, dry (without propfan), kg 103
Dimensions, mm 1,085 х 536 х 515
Specified service life, h 3,000


  • Ка-226