| Aircraft Engine Manufacturer |
Daimler-Benz |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
498.498 |
| Length (mm) |
116.84 |
| Height (mm) |
196.85 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Mercedes_D.IVa |
| Fuel |
Gasoline |
| Fuel System |
Twin jet Mercedes carburettor with automatic mixture control |
| Oil System |
Forced feed to bearings and camshaft |
| Cylinders |
6 |
| Cylinders Disposition |
inline |
| Bore (mm) |
160 |
| Stroke (mm) |
180 |
| Displacement (L) |
21.72 |
| Compression Ratio |
4.94 |
| Valvetrain |
Shaft driven SOHC operating twin exhaust and inlet valves with a half compression setting for starting |
| Cooling |
Water-cooled |
| Maximum Takeoff Power (kW) |
187.9164 |
| Power To Weight (kW/kg) |
0.376 |
| Specific Fuel Consumption (g/(kW·h)) |
329.1 |