Ivchenko-Progress AI-322

The Ivchenko-Progress AI-322 (Ukrainian: AI-322, Russian: АИ-322) are a family of low-bypass turbofan engines developed from the AI-222 engine.

Design and development

The development of the engine continues at Ivchenko-Progress of Zaporizhzhia, Ukraine. The engine was originally intended for the Hongdu L-15 trainer aircraft and it is now planned to be used in Baykar Bayraktar Kızılelma fighter UAV. An afterburning version, the AI-322F is also available.

Data from

Type: Two-spool low-bypass turbofan
Length: 1,960 mm (77 in)
Diameter: 640 mm (25 in)
Dry weight: 440 kg (970 lb) in base configuration, 560 kg (1,230 lb) in afterburning configuration

Maximum thrust: 2,500 kgf (24.5 kN; 5,511.6 lbf) in takeoff mode (non-afterburning), 4,200 kgf (41.2 kN; 9,259.4 lbf) afterburning.
Overall pressure ratio: 15.43:1
Bypass ratio: 1.19:1
Turbine inlet temperature: 1,470 K (1,200 °C)
Fuel consumption: 0.66 kg/kgf.h (18.7 g/kNs) (non-afterburning), 1.9 kg/kgf.h (53.8 g/kNs) (afterburning)
Specific fuel consumption: 0.66 kg/(kgf h)
Thrust-to-weight ratio: 5.68 (non-afterburning), 7.5 (afterburning)

↑ "Motorsich AI-222-25F". Archived from the original on 2022-11-24. Retrieved 2022-11-24.

v t e Ivchenko-Progress aircraft engines
Piston engines	AI-4 AI-14 AI-26
Turboshafts/turboprops and auxiliary power units (APU)	AI-8 AI-9 AI-20 AI-24 AI-450 D-136
Turbofans and propfans	AI-22 AI-222 AI-25 AI-322 DV-2 D-18T D-27 D-36 D-236 D-436 MS-400
Turbojets	PBS AI-PBS-350