Applications
Antonov An-2
Antonov An-6
Lissunov Li-2
De Havilland Canada DHC-3
Neman R-10
Polikarpov I-153
Polikarpov I-16
PZL-106 Kruk (some variants)
PZL M18 Dromader
PZL M24 Dromader Super (K-9AA)
Sukhoi Su-2
Sukhoi Su-12
Technical data (M-62)
Characteristic data
Cylinder 9, air-cooled, single-row star arrangement
Hole 156 mm
Stroke 175 mm
Cubic capacity 29.8 l
Length 1213 mm
Diameter 1378 mm
Weight 560 kg
Two-stage supercharging compressor
Fuel system carburetor
Fuel gasoline, at least 92 octane. (Usually AvGas 100 LL is prescribed).
Output 746 kW (1,014.3 hp) at 2200 rpm take-off power.
634 kW (862 hp) at 2100 rpm at 4200 m altitude.
Compression ratio 6.4: 1
Power / weight ratio 1.3 kW / kg