Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: JSC KMPO
Parent System: NK-93
Initial Operational Capability (IOC):
Total Production: ?
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Description: The NK-93A is a low consumption, high by-pass ratio turbofan engine designed to power next-generation Russian airplanes such as the Tu-330 cargo transport aircraft. The NK-93A develops 20,000 kg (44,091 pounds) of thrust at take-off.

The NK-93A engine is an alternative engine for military versions of the Tu-330 cargo transport aircraft. The Tu-330 powered by tow NK-93s will have greater flight range than Tu-330 powered by PS-90A engines.

NK-93A Applications

Support Aircraft Tu-330

NK-93A Specifications

Fan Diameter: 2,900 millimeter (114 inch)
Length: 5,972 millimeter (235 inch)
Dry Weight: 3,650 kilogram (8,047 pound)
Max Cruise Thrust: 3,300 kilogram
Max Takeoff Thrust: 44,091 pound (20,000 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)
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