Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: Klimov JSC and MMP Chernyshev
Parent System: RD-33
Initial Operational Capability (IOC): 1984
Total Production: ?
Family Members: RD-33, RD-33 OVT, RD-33MK and RD-93MA
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Description: The Klimov RD-33 is a family of fighter aircraft engines developed to power the Mig-29 multi-role fighter and delivering between 18,000 and 20,000 pounds of thrust. Despite the Soviet Union's collapse, RD-33 engine family has evolved encompassing cutting technologies such as thrust vectoring control (TVC) which provides superior aircraft maneuverability compared with fixed nozzles engines.

The RD-33K is an improved variant of RD-33 engine providing around 1,000 pounds of additional thrust. This new variant was available as standard equipment for Mig-29M, Mig-29M2, Mig-29K and Mig-29SMT aircraft. Each RD-33K engine is rated at 19,400 pounds of thrust.

RD-33K Applications

Combat Aircraft Mig-29K Mig-29M Mig-29M2 Mig-29SMT

RD-33K Specifications

Thrust: 19,400 pound (8.80 ton)
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


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