RD-93MA  
Initial Operational Capability (IOC): 2016
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-33K and RD-33MK
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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-93MA is a more powerful variant of the RD-93 engine powering the FC-1/JF-17 fighter aircraft. The RD-93MA develops 9,300kg of thrust and is intended to power improved FC-1/JF-17 jets.

RD-93MA Applications


Combat Aircraft FC-31

RD-93MA Specifications

Weight
Max Thrust with Afterburning: 9,300 kilogram (20,503 pound)
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


OperatorsItems

Grand Total ?2
 
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