Klimov M-103 Piston Engine

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Aircraft Engine Manufacturer
Klimov
Aircraft Engine Type
Piston
Dry Weight (kg)
500
Length (mm)
197.1
Height (mm)
94.2
Width (mm)
76.4
Wikipedia Article (URL)
en.wikipedia.org/wiki/Klimov_M-103
Fuel
90 (minimum grade), 95 or 100 octane.
Fuel System
Six K-100A carburettors (license copy of Solex-Hispano 56S2 self-adjusted carburettor)
Cylinders
12
Bore (mm)
148
Stroke (mm)
170
Displacement (L)
35.1044
Supercharger
Gear-driven single-speed centrifugal type compressor. Gear ratio: 11.0:1. Maximum boost for take-off: . Maximum boost at altitude: . Critical altitude:
Compression Ratio
6.6
Valvetrain
One intake and one sodium-filled exhaust valve per cylinder actuated via a single overhead camshaft per bank.
Cooling
Liquid-cooled
Specific Power (kW/L)
21.22
Power To Weight (kW/kg)
1.5
Specific Fuel Consumption (g/(kW·h))
199514.9

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