Stuff You Can Buy
 
 
 
Other Stuff
 
 

Pratt & Whitney J75 (JT4)

The Engine Specifications
 
The J75 was a scaled up J57 and first flew in 1955.  This turbojet was in production from 1956 through 1967.
Turbojet
Dual compressor, axial flow
mass flow: 249-256 lbs/sec
 
Models Used by
 
YJ75-P-11: 23,500 lb (104.5 kN) afterburning thrust
J75-P-17: 24,500 lb (109 kN) afterburning thrust
J75-P-19W: 24,500 lb (109 kN) afterburning thrust
Republic F-105 Thunderchief
Convair F-106 Delta Dart
North American F-107
Martin P6M Seamaster
 
Related Pages
 
More about Pratt & Whitney
 

page updated 04 July 2003

 

 

Use of photographs | References  | Disclaimer | Privacy

 
   

Apple iTunes

free counters

   

Kenneth W Shanaberger 2000 - 2010