| Mercedes D.II ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Daimler-Benz |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 210 |
| Length (mm) | 165 |
| Height (mm) | 107.2 |
| Width (mm) | 49 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Mercedes_D.II |
| Cylinders | 6 |
| Cylinders Disposition | inline |
| Bore (mm) | 125 |
| Stroke (mm) | 150 |
| Displacement (L) | 11.05 |
| Compression Ratio | 4 |
| Valvetrain | Single overhead camshaft (SOHC) with two valves per cylinder |
| Cooling | Liquid |
| Maximum Takeoff Power (kW) | 89.484 |