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RD-33
IOC: 1984
RD-33K
Origin Russia
Contractor/s
Klimov JSC MMP Chernyshev
Applications
Mig-29K Mig-29M Mig-29M2 Mig-29SMT
Family Members
RD-33 RD-33 OVT RD-33MK
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Description:
Klimov RD-33 is a family of aircraft engine 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.
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.
Specifications
Engine/s Performance: Thrust 19,400 lb (8,800 kg)
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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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