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Pratt & Whitney Engines
F100-PW-229 TURBOFAN ENGINE

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Aircraft used on (click here)

 

Engine Characteristic

Maximum Thrust (Full Augmentation) 29,100 lb (129.4 kN)
Intermediate Thrust (Nonaugmented) 17,800 Ib (79.2 kN)
Weight (Specification Maximum) 3,740 lb (1,681 kg)
Length 191 in. (4.85 m)
Inlet Diameter 34.8 in. (0.88 m)
Maximum Diameter 46.5 in. (1. 18 in)
Bypass Ratio 0.36
Overall Pressure Ratio 32 to 1

 

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