| Aircraft Engine Manufacturer |
Junkers |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
1088 |
| Diameter (mm) |
116 |
| Length (mm) |
240 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Junkers_Jumo_222 |
| Fuel System |
Fuel injection |
| Cylinders |
24 |
| Cylinders Disposition |
in-line |
| Bore (mm) |
135 |
| Stroke (mm) |
135 |
| Displacement (L) |
46.38 |
| Supercharger |
Single-stage two-speed centrifugal type supercharger |
| Compression Ratio |
6.5 |
| Valvetrain |
Two intake valves and one sodium-cooled exhaust valve per cylinder |
| Cooling |
Liquid-cooled |
| Maximum Takeoff Power (kW) |
1838 |
| Specific Power (kW/L) |
39.5 |
| Power To Weight (kW/kg) |
1.69 |
| Specific Fuel Consumption (g/(kW·h)) |
176.4 |