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RM12  
Initial Operational Capability (IOC): 1997
Total Production: ?
Origin: Sweden and United States of America
Corporations: General Electric and Volvo Aero
Parent System: RM12
Initial Operational Capability (IOC): 1997
Total Production: ?
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Description: The RM12 engine is a derivative of the proven General Electric F404 engine used on the F/A-18 aircraft family to power the single engine JAS 39 multi-role fighter and all variants (B/C/D models). Thus, the engine features and performance are very similar to those of the F404 engines. RM12 modifications focus on optimized performance and reliability for single-engine aircraft operations.

The RM12 is produced jointly between General Electric Aircraft Engines and Volvo Aero Corporation from Sweden. SAAB JAS-39 Gripen multi-role fighters ordered by Sweden and international customers are powered by one RM12 jet engine.

RM12 Applications


Combat Aircraft JAS 39C Gripen JAS 39D Gripen

RM12 Specifications

Dimensions
Fan Diameter: 890 millimeter (35.0 inch)
Length: 3.91 meter (154 inch)
Weight
Dry Weight: 1,055 kilogram (2,326 pound)
Thrust: 18,100 pound (8.21 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


OperatorsItems

Grand Total ?5
 
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