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Allison J71 Turbojet

The Engine Specifications
 
In 1948, Allison began a complete redesign of their successful J35.  Originally designated the J35-A-23, this engine was later re-designated the J71.
Turbojet
16-stage compressor
3-stage turbine
Mass flow: 160 lbs/sec
Pressure ratio: 8
 
Models Used by
 
J71-A-2E: 9,700 lb (43.1 kN) thrust (14,000 lb (62.3 kN) thrust with afterburner)
J71-A-11: 10,200 lb (45.4 kN) thrust
McDonnell F3H Demon
Douglas B-66 Destroyer
 
Related Pages
 
More about Allison
 

page updated 04 July 2003

 

 

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Kenneth W Shanaberger 2000 - 2010