General Electric F404

Turbofan · General Electric Company
Reaction Turbines
Bypass Ratio
0.34
Diameter
889 mm
Length
3910 mm
Dry Weight
1035.098 kg
Thrust To Weight
4.8

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber Annular
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 0.34 Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Boeing Phantom Ray General Electric F404 1 10.9728 15.24
Boeing–Saab T-7 Red Hawk General Electric F404 1 14.0208 9.144
FMA SAIA 90 General Electric F404 2 15.53 10.95
HAL Tejas General Electric F404 1 13.2 8.2
KAI T-50 Golden Eagle General Electric F404 1 13.14 9.45
TAI Hürjet General Electric F404 1 13.6 9.5
All data (15 fields)
Name
General Electric F404
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1035.098
Diameter (mm)
889
Length (mm)
3910
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_F404
Geared Fan
No
Combustion Chamber
Annular
Afterburner
Yes
Streams
2
Bypass Ratio
0.34
Thrust To Weight
4.8
Compressor Description
Axial, with 3 Fan and 7 HP stages
Turbine Description
1 LP and 1 HP stage