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Pratt & Whitney T34

The Engine Specifications
 
In 1945, P&W began development of a U.S. Navy funded turboprop, the T34.  First flown in 1950, the T24 was in production from 1951 through 1960.
Axial-flow turboprop
13 stage compressor
3 stage turbine
Mass flow: 65 lbs/sec
pressure ratio: 6.7
 
Models Used by
 
T34-P-3: 6,000 hp (4469 kw)
T34-P-7W: 7,100 hp (5288 kw) w/water injection
T34-P-9W: 7,500 hp (5586 kw) w/water injection
Douglas C-133 Cargomaster
 
Related Pages
 
More about Pratt & Whitney
 

page updated 04 July 2003

 

 

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Kenneth W Shanaberger 2000 - 2010