Initial Operational Capability (IOC): 1980
Total Production: ?
Origin: Russia
Corporations: Aviadvigatel Perm Engine Company and NPO Saturn
Parent System: D-30
Initial Operational Capability (IOC): 1975
Total Production: ?
Family Members: D-30KP
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Description: The D-30 is a family of turbofan engines developed and manufactured in the former Soviet Unit to power a wide range of jet aircraft ranging from fighters to tactical transport jets. There is a power generator application known as D-30STU based on the D-30 gas turbine. The engine family develops between 25,000 to 35,000 pounds of thrust. As of 2005, D-30 engines are being manufactured and marketed by Russian corporations NPO Saturn and Aviadvigatel.

The D-30F6 two-shaft engine provides 15,500 kg of thrust with afterburning and was selected to power the high-speed supersonic Mig-31 Foxhound air defense interceptor. The D-30F6 engine enables Mig-31 to fly at high altitudes and airspeeds of Mach 2.8 while performing air defense patrols. The engine design consists of 7 line replaceable modules. Sukhoi's S-37 Berkut Forward Swept Wing aircraft demonstrator was powered by two D-30F6 engines as well.

D-30F6 Applications

Combat Aircraft Mig-31 Mig-31BM

D-30F6 Specifications

Dry Weight: 2,416 kilogram (5,326 pound)
Max Takeoff Thrust: 9,500 kilogram (20,944 pound)
Max Thrust with Afterburning: 15,500 kilogram (34,171 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


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