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Pratt & Whitney Engines
F119-PW-100 TURBOFAN ENGINE

Aircraft using this engine (click here)

Engine Characteristic
Type	Twin-Spool, Augmented Turbofan
Application	F-22 Advanced Tactical Fighter
Thrust	35,000 Pound Thrust Class
Engine Control	Full-Authority Digital Electronic Control
Compression System	Twin Spool/Counter Rotating/Axial Flow/ Low-Aspect Ratio      Three-Stage Fan      Six-Stage Compressor
Combustor	Annular
Turbine	Axial Flow/Counter Rotating • One-Stage, High-Pressure Turbine • One-Stage, Low-Pressure Turbine
Nozzle	Two-dimensional Vectoring Convergent/Divergent

 

This material is copyrighted to Pratt and Whitney and they retain and reserve all rights to this material.  The use of this material by the ALLSTAR network is with permission of Pratt and Whitney.  The ALLSTAR network's copyright applies to the format used in presenting this material.  Pratt and Whitney should be contacted directly for permission to use this material.

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Updated: March 12, 2004