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NK-93
NK-93A
Origin
Russia
Program Status:
Under Development
Contractor/s
JSC KMPO
Applications
Tu-330
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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.
Specifications
Dimensions: Fan Diameter 2,900 mm, Length 5,972 mm
Weights: Dry Weight 3,650 kg (8,047 lb)
Engine/s Performance: Max Cruise Thrust 3,300 kg (7,275 lb), Max Takeoff Thrust 44,091 lb (20,000 kg)
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Saturday, November 22, 2008
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