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Pratt & Whitney F100

The Engine  Specifications
 
The F100 was designed for the F-15 Eagle and first flew on that aircraft in 1972.  The F100 had developmental problems when it was first introduced but today is one of the most reliable fighter engines in the world.
Turbofan
Bypass ratio: .34
Fan: 3-stage
Compressor: 10-stage HP
Turbine: 2-stage HP, 2-stage LP
Pressure ratio: 35
 
 Models  Used by
 
F100-PW-100: 23,930 lb (106 kN) afterburning thrust
F100-PW-200: 23,770 lb (105.7 kN) thrust
McDonnell Douglas F-15 Eagle
General Dynamics F-16 Fighting Falcon
 
 Related Pages  Related Websites
 
More about Pratt & Whitney
Pratt & Whitney: F100
 

page updated 09 March 2006

 

 

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Kenneth W Shanaberger 2000 - 2010