Initial Operational Capability (IOC):
United Engine Corporation
Parent System: PD-35
Initial Operational Capability (IOC): 2025
Total Production: ?
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Description: The United Engine Corporation PD-35 is an advanced aviation turbofan engine developed to power a wide array of new generation wide-body airplanes including the CR929 wide-body airliner. The PD-35 incorporates some technologies introduced on the PD-14 turbofan engine developed for the MC-21 narrow body airliner. The PD-35 is more powerful than the alternative engines provided to current Russian-made aircraft. The project started in 2016 and the new engine is slated to enter service in the 2023-2025 timeframe. Russia is also planning to use the 77,000-lb of thrust engine to power a variety of other aircraft including wide-body military transport airplanes.
Fan Diameter: 3.10 meter (122 inch)
Length: 8 meter (315 inch)
Dry Weight: 8,000 kilogram (17,637 pound)
Max Takeoff Thrust: 77,000 pound (34,927 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)
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on 24 Sep 2017
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