Tumanskii R-29

Stuff You Can Buy

Other Stuff

Use of photographs | References | Disclaimer | Privacy

© Kenneth W Shanaberger 2000 - 2010

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