PD-24  
Initial Operational Capability (IOC): 2025
Total Production: ?
Also Known As: PD-28
Origin: Russia
Corporations: United Engine Corporation
Parent System: PD-24
Initial Operational Capability (IOC): 2025
Total Production: ?
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Description: The PD-24 and PD-28 are two turbofan engines developing between 54,000 pounds and 63,000 pounds of thrust and derived from the United Engine Corporation PD-14 turbofan. These engines may be intended to power a new generation of regional wide-body airliners or military aircraft.

PD-24 Specifications

Weight
Max Takeoff Thrust: 54,000 pound (24,494 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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
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