Aircraft engine: Lyulka AL-21F3
USSR
jet engine
Configuration | single-spool axial-flow turbojet with 14-stage compressor, annular combustion chamber, 3-stage turbine and afterburner | Weight | 1,720 kg (3,792 lb) | Maximum dry thrust | 78 kN (17,535 lbf) | Maximum thrust with afterburner | 111.5 kN (25,066 lbf) |
The engine was designed at Lyulka Design Bureau in late 1960s. It is used in MiG-23B, Su-17, Su-20, Su-22 and Su-24 combat aircraft.
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