Mikulin AM-35

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The Mikulin AM-35 was a 1930s Soviet aircraft piston engine. Derived from the AM-34FRN, AM-35 entered production in 1940 and was used on MiG-1 and MiG-3 World War II fighters as well as the Petlyakov Pe-8 heavy bomber. The engine was very similar to the AM-38F of the Il-2 Shturmovik, and built in the same plant (Kuybyshev, in late 1941); this was the reason of the end of its production, as Mikulin was forced to focus production on the AM-38F.

[edit] Specifications (AM-35A)

General characteristics

• Type: 12-cylinder 60° Vee aircraft piston engine
• Bore:
• Stroke:
• Displacement: 46.66 L (2,847 in³)
• Length: 2402 mm (94.5 in)
• Width: 866 mm (34.1 in)
• Height: 1089 mm (42.9 in)
• Dry weight: 830 kg (1,830 lb)

Components

• Supercharger: Two-speed centrifugal type M-100 with aftercooler
• Cooling system: Liquid-cooled

Performance

• Power output: 993 kW (1,350 hp) at 2,050 rpm
• Specific power: 21.6 kW/L (0.47 hp/in³)
• Compression ratio: 7.0:1
• Specific fuel consumption: 0.46 kg/km (1.64 lb/mile) caclulated, 0.38 kg/km (1.35 lb/mile) observed.
• Power-to-weight ratio: 1.21 kW/kg (0.74 hp/lb)