WS-20  
Initial Operational Capability (IOC): 2017
Maiden Flight: 2013
Total Production: ?
Origin: China
Corporations: Aero Engine Corp of China
Parent System: WS-20
Initial Operational Capability (IOC): 2016
Total Production: ?
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Description: The WS-20, also known as WS-188, high-by-pass ratio turbofan engine designed to power the Y-20 heavy-lift transport aircraft and designed to develop up to 13,800 kg of thrust at takeoff. The WS-20 engine is a derivative of the WS-10A fighter jet engine utilizing the same core. The engine was first seen in 2014 and entered service in 2016/2017 powering the Y-20 aircraft.

WS-20 Applications


Airliners Y-20F-100 Support Aircraft Y-20

WS-20 Specifications

Weight
Max Takeoff Thrust: 13,800 kilogram (30,423 pound)
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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
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