Mikulin AM-39
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.
Mikulin AM-39 | |
---|---|
Type | Liquid-cooled V-12 piston engine |
Manufacturer | Mikulin |
First run | 1942 |
Major applications | Mikoyan-Gurevich I-220 |
Developed from | Mikulin AM-35 |
Specifications (AM-39FN)
Data from Kotelnikov'.[1]
General characteristics
- 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)
Components
- Supercharger: Two-speed centrifugal type supercharger with aftercooler
- Fuel system: Direct injection
- Cooling system: Liquid-cooled
References
Notes
- Kotelnikov 2005, p. 112.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.