The Mikulin AM-39 was a 1940s Soviet aircraft piston engine. Representing a high-output version of the AM-35A, AM-39 was used on the Mikoyan-Gurevich I-220 and Polikarpov ITP fighters, and the Tupolev SDB bomber.
|Type||Liquid-cooled V-12 piston engine|
|Major applications||Mikoyan-Gurevich I-220|
|Developed from||Mikulin AM-35|
- Type: 12-cylinder 60° Vee aircraft piston engine
- Bore: 160 mm (6.30 in)
- Stroke: 190mm/196.7mm (7.48 in/7.744 in) different between right and left cylinder bank due to articulated connecting rods
- Displacement: 46.66 L (2,847 in³)
- Dry weight: 970 kg (2,138 lb)
- Supercharger: Two-speed centrifugal type supercharger with aftercooler
- Fuel system: Direct injection
- Cooling system: Liquid-cooled
- Power output: 1,588 kW (2,130 hp)
- Specific power: 34 kW/L (0.75 hp/in³)
- Kotelnikov 2005, p. 112.