Wednesday, December 03, 2008

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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

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)

Operators

see operators map | see family operators map

Russia
Sudan
Yemen

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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