| Thursday, August 28, 2008 |
 |
F404
IOC: 1980
Total Production: 3,700
F404-GE-402
IOC: 1992
Origin:United States of America
Contractor/s:
General Electric
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.
The F404-GE-402 engine retains the characteristics of baseline F404, while achieving higher power and increased fuel efficiency. This increased performance is the result of applying the latest technology and materials to the turbine and afterburner sections.
F404-GE-402 engines were installed on production F/A-18C/D Hornet since 1992.
Specifications
Dimensions: Diameter 890 mm, Length 3.9 m
Weights: Max Weight 1,035 kg (2,282 lb)
Engine/s Performance: Thrust 17,700 lb (8,029 kg)
|
|
Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Sunday, August 24, 2008
Leave Feedback >>
|
|
Copyright © 2003 - 2008 deagel.com. All Rights Reserved.