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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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© 1995-99 ALLSTAR Network. All rights reserved worldwide.
Funded in part by | Used with permission from Pratt & Whitney |
Updated: February 23, 1999