NK-32  
Initial Operational Capability (IOC): 1987
Maiden Flight: 1981
Total Production: 240
Also Known As: NK-231
Origin: Russia
Corporations: ND Kuznetsov
Parent System: NK-32
Initial Operational Capability (IOC): 1987
Maiden Flight: 1981
Total Production: 440
Family Members: NK-32.02
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Description: The NK-32 turbofan engine, also referred to as the NK-231, was developed in the 1980s to power the Soviet Union's Tu-160 strategic bomber. The engine features 30,000-lb of thrust non-afterburning and 55,000-lb with afterburner. The NK-231 engine features fuel consumption optimization providing supersonic speed as well as intercontinental range.

NK-32 Applications


Combat Aircraft Tu-160 Tu-160M

NK-32 Specifications

Weight
Max Thrust non-Afterburning: 30,865 pound
Max Thrust with Afterburning: 55,100 pound (24,993 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)

NK-32 News

There are 3 news between
17 Jul 2015 and 22 Jun 2017
Thursday, June 22, 2017Russian Air Force Tu-160M2 Bomber to Take to the Skies in March 2018
Monday, August 15, 2016Russia to Produce First Modernized Tu-160M2 NK-32.02 Engines by End of 2016
Friday, July 17, 2015Tu-160M2 Bomber to Feature Hypersonic Cruise Missiles and Upgraded NK-32 Engine

Operators & Related Equipment


OperatorsItems
Russia240

Grand Total 2402
 
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