NK-123 turboshaft by Samara NTK

In year 2000 new engine project entered stage of technical/assembly documentation. Mass production is expected to start in 2004. NK-123 is intended for light aircraft Il-100 and some new helicopters.

  • ModelRD-33

    Year 2004?
    Type Turboshaft
    Takeoff
    Power 650hp
    Fuel consumption?kg/hp/hour
    Cruise
    power ?hp
    Fuel consumption0.223kg/hp/hour
    other parameters
    Resource (between repair)5000h
    Length ?mm
    Maximum Diameter?mm
    Weight ?kg
  • The NK-123 project
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