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Tumanskii R-29

The Engine Specifications
 
Introduced in 1972, the R-29 was as refined version of the R-27 designed by Khachaturov of the Tumanskii construction bureau.  The R-29 features both afterburning and water injection.
Turbojet
Compressor: 5-stage LP/6-stage HP
Turbine: 1-stage HP/2-stage LP
 
Models Used by
 
R-29B-300: 25,335 lb (112.7 kN) afterburning thrust
MiG-23MF "Flogger"
MiG-27M "Flogger"
 
Related Pages
 
More about Tumanskii
 

page updated 19 July 2003

 

 

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Kenneth W Shanaberger 2000 - 2010