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AI-222

The engines have been optimized to be operated on up-to-date trainer, combat trainer, and light combat aircraft and unmanned aerial vehicles it complies with strict requirements for the engines of this class.
Using the AI-222 family engines will allow creating a number of highly competitive aircraft.
At customer’s request, all the AI-222 engines can be equipped with vectored thrust nozzles or their versions with afterburners can be developed.

Main advantages of the engine:

  • High reliability;
  • Optimum performance;
  • Low noise, emission, and infrared signature;
  • Long service life;
  • Low operating costs.

Basic specifications:

Specifications AI-222-25 AI-222-28
Maximum power condition (SLS, ISA, σin=1,0):
Thrust, kgf (kN)
(flat-rated to tAMB=+30°C)
2500 (24.52) 2800 (27.47)
SFC,kg/kgf•h (kg/kN•h) 0.64 (65.2) 0.67 (68.3)
Maximum power condition Hn=5000 m; Mn=0,6;
ISA;
σin=0,97)
Hn=5000 m; Mn=0,6;
ISA;
σin=0,97)
Thrust, kgf (kN) 1450 (14.22) 1550 (15.21)



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Applicability


  • L-159
  • Yak-130

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