The engine is developed from a version of the AI-222-25.
Length - 2020 mm
Engine diameter - 630 mm
Weight - 520 mm
Specific power consumption 0,67 kg/kgf-hr
Bypass ratio 1.13:1
Turbine inlet temperature - 1320°C
Max. take-off thrust - 27,74 kN
Source:
http://aviaros.narod.ru/ai-222.htm
Length - 2020 mm
Engine diameter - 630 mm
Weight - 520 mm
Specific power consumption 0,67 kg/kgf-hr
Bypass ratio 1.13:1
Turbine inlet temperature - 1320°C
Max. take-off thrust - 27,74 kN
Source:
http://aviaros.narod.ru/ai-222.htm