AI-322-30 Turbofan


Turbojet engine AI-322-30 is designed for use on modern training and light combat aircraft.

Maximum Power (SLS, ISA σin=1)
Thrust, kgf (maintained up to tamb = + 30°С)

3,000

Specific fuel consumption, kg/kgf/h 0.70
Maximum power (H = 5,000 m; M = 0.6; ISA; σin=0.97)
Thrust, kgf 1,610
Maximum cruise power (H = 10,000 m; M = 0.6; ISA; σin=0.97)
Thrust, kgf(maintained up to tamb = + 30°С) 590
Specific fuel consumption, kg/kgf/h 0,84
Fan diameter, mm 624
Dimensions (without inlet fairing), mm 3,138 х 860 х 1,096
Weight, dry, kg 534