АI-322F Turbofan Aero Engine with Afterburner


Designed to power modern supersonic trainers, training-combat and light combat aircraft operated at moderate supersonic speeds (up to M=1.6). Installed on the L-15 LIFT.

Full afterburning power (SLS, ISA)
Thrust, kgf 4,200
Specific fuel consumption, kg/h/kgf 1,9
Full afterburning power (H=11,000 m, М=1,4; ISA, σin=0,97)
Thrust, kgf 2 760
Maximum (SLS, ISA)
Thrust, kgf 2,500
Specific fuel consumption, kg/kgf/h 0,66
Dimensions (without inlet fairing), mm 3,070 х 880 х 1,084
Weight, dry, kg 560

Applicability


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