| Aircraft Engine Manufacturer |
BMW |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
1012 |
| Diameter (mm) |
129 |
| Length (mm) |
200.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/BMW_801 |
| Fuel System |
Direct fuel injection |
| Cylinders |
14 |
| Cylinders Disposition |
radial |
| Bore (mm) |
156 |
| Stroke (mm) |
156 |
| Displacement (L) |
41.8 |
| Supercharger |
Gear-driven single-stage two-speed |
| Compression Ratio |
6.5 |
| Valvetrain |
One intake and one sodium-cooled exhaust valve per cylinder |
| Cooling |
Air-cooled, with oil cooler integrated into forward cowl |
| Maximum Takeoff Power (kW) |
1147.378 |
| Specific Power (kW/L) |
27.44 |
| Power To Weight (kW/kg) |
1.13 |
| Specific Fuel Consumption (g/(kW·h)) |
187.3 |