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The Teledyne CAE F408 is an American turbofan engine developed for a number of UAVs, drones, and cruise missiles in the late 1980s.

Design and development

The F408 (Model number 382-10) is a bypass turbofan whose fan stage is followed by a mixed-flow compressor, slinger-type combustor, and single-stage turbine. The turbine design is similar to that of the earlier Model 373-8B, while the compressor and fan are more advanced in design.

The development of the F408 began in 1985, with test runs beginning in 1989.

Applications

• BQM-145 Peregrine
• Eclipse 500 (first prototype)

Specifications

Data from

General characteristics

• Type: Turbofan
• Length: 32.1 in (81.5 cm)
• Diameter: 13.2 in (33.5 cm)
• Dry weight: 143.30 lb (65.8 kg)

Components

• Compressor: Mixed flow compressor
• Combustors: Slinger
• Turbine: Single stage high pressure turbine

Performance

• Maximum thrust: 998.69 lbf (4.44 kN)
• Specific fuel consumption: 1.2 lb/(lbf⋅h) or 34 g/(kN⋅s)

References

1. Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1.
2. ^ "Teledyne CAE F408-CA-400". Minijets. 24 July 2022.
3. "Designations Of U.S. Military Aero Engines". www.designation-systems.net.
4. "Eclipse 500 - CAE-F408". Minijets. Archived from the original on 2019-10-17. Retrieved 2020-04-03.

• Teledyne Technologies
• 1980s turbofan engines