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Initial Operational Capability (IOC):
Origin: United States of America
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Description: The F404 engine was developed to power the US Navy's F/A-18 Hornet. It has been proved as a reliable high performance engine. The F404 incorporates an array of new technologies, modular design and advanced materials.
This engine allows to carry out a wide spectrum of missions from low level attack to high altitude interceptors. The F404-GE-400 engine can be assembled/disassembled in short time, making it an easy to maintain engine.
Fan Diameter: 890 millimeter (35.0 inch)
Length: 3.91 meter (154 inch)
Dry Weight: 991 kilogram (2,185 pound)
Thrust: 16,000 pound (7.26 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)
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on 12 Jan 2009
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