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.

models

• R-29B-300: 25,335 lb (112.7 kN) afterburning thrust

specifications

• Turbojet
• Compressor: 5-stage LP/6-stage HP
• Turbine: 1-stage HP/2-stage LP

used by

• MiG-23MF "Flogger"
  MiG-27M "Flogger"