| Aircraft Engine Manufacturer |
HuoSai |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
560 |
| Diameter (mm) |
137.8 |
| Length (mm) |
121.3 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Shvetsov_ASh-62 |
| Fuel |
92 RON, 87 (R+M)/2 (AKI) octane rating gasoline |
| Fuel System |
Carburetor |
| Cylinders |
9 |
| Cylinders Disposition |
radial |
| Bore (mm) |
155.5 |
| Stroke (mm) |
174 |
| Displacement (L) |
29.876 |
| Supercharger |
Two-speed centrifugal type supercharger |
| Compression Ratio |
6.4 |
| Valvetrain |
Overhead valves |
| Cooling |
Air-cooled |
| Maximum Takeoff Power (kW) |
746 |
| Specific Power (kW/L) |
25.03 |
| Power To Weight (kW/kg) |
1.3 |
| Specific Fuel Consumption (g/(kW·h)) |
285281.9 |