Teledyne CAE F408

Turbofan · Lycoming
Reaction Turbines
Maximum Takeoff Thrust
4.44 kN
Diameter
335.28 mm
Length
815.34 mm
Dry Weight
64.9998 kg

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 Slinger
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 — Overall Pressure Ratio — Afterburner No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
BQM-145 Peregrine Teledyne CAE F408 1 5.6 3.2

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN)
Ishikawajima Ne-20 IHI Corporation 4.6 Compare
All data (14 fields)
Name
Teledyne CAE F408
Aircraft Engine Manufacturer
Lycoming
Aircraft Engine Type
Turbofan
Dry Weight (kg)
64.9998
Diameter (mm)
335.28
Length (mm)
815.34
Wikipedia Article (URL)
en.wikipedia.org/wiki/Teledyne_CAE_F408
Geared Fan
No
Combustion Chamber
Slinger
Afterburner
No
Streams
2
Maximum Takeoff Thrust (kN)
4.44
Compressor Description
Mixed flow compressor
Turbine Description
Single stage high pressure turbine