Initial Operational Capability (IOC):
Origin: United States of America
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Description: The F404-GE-IN20 is a variant of F404-GE-402 engine designed to meet the requirements of the Indian Air Force and Navy for the Tejas, formerly LCA, combat aircraft. Modifications introduced into the -IN20 engine include redundant features and an advanced Full Authority Digital Electronic Control (FADEC).
The Indian ADA agency awarded General Electric a $105 million contract in February 2004 for development engineering and production of 17 F404-GE-IN20 engines. The Indian Air Force will take delivery of its first -IN20 engines in 2006. These engines will be used to power low rate (also called limited) production Tejas/LCA aircraft.
Fan Diameter: 890 millimeter (35.0 inch)
Length: 3.91 meter (154 inch)
Dry Weight: 1,035 kilogram (2,282 pound)
Thrust: 20,200 pound (9.16 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)
There are 3 news between
5 Feb 2004 and 6 Jul 2010
Operators & Related Equipment
Engines ordered to power Tejas aircraft
Grand Total 411
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