| Aircraft Engine Manufacturer |
Renault |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
205 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Renault_6P |
| Fuel |
80 Octane gasoline |
| Oil System |
Pressure fed, 3.0 kg/cm2, dry sump |
| Cylinders |
6 |
| Cylinders Disposition |
in-line |
| Bore (mm) |
120 |
| Stroke (mm) |
140 |
| Displacement (L) |
9.5 |
| Compression Ratio |
5.75 |
| Valvetrain |
Pushrod-actuated, single intake and single exhaust valve per cylinder |
| Cooling |
Air |
| Maximum Takeoff Power (kW) |
134.226 |
| Power To Weight (kW/kg) |
0.654 |
| Specific Fuel Consumption (g/(kW·h)) |
203.8 |