AI-450-2 Turboshaft


The AI-450-2 engine is designed for use on light multi-purpose helicopters. The AI-450-2 is developed on the basis of the Ivchenko-Progress AI-450 turboshaft gas turbine engine.

2.5 min power (SLS, ISA)
Output shaft power, h.p. (maintained at up to t=+300C), min. 800
30 min power (SLS, ISA)
Output shaft power, h.p. (maintained at up to t=+300C), min. 750
Takeoff Power (SLS, ISA)
Output shaft power, h.p. (maintained at up to t=+3500C), min. 630
Cruise Power
Output shaft power, h.p. (maintained at up to t=+300C), min. 450
Specific fuel consumption. kg/hp/h 0.3
Weight, dry, kg 125
Dimensions, mm 1149 х 520 х 567