Pratt & Whitney F100

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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

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page updated 09 March 2006