Wednesday, December 03, 2008

AL-41

IOC: 2010

Origin
Russia

Contractor/s
NPO Saturn

Applications
PAK FA

Description: Te AL-41 is a 40,000-lb class engine being designed to power Russian fifth generation aircraft. It features Thrust Vectoring Control (TVC), advanced materials, optimized radar cross section and IR signatures for stealth, Fully Authority Digital Engine Control (FADEC).

The AL-41 engine is a follow-on of the proven AL-31 which powers Su-27 family aircraft. It would power both single and twin engine aircraft.

Specifications
Engine/s Performance: Thrust 40,000 lb (18,144 kg)

Image Gallery

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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