| Renault 70 hp ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Renault |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 179.6226 |
| Length (mm) | 115.57 |
| Height (mm) | 83.312 |
| Width (mm) | 75.692 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Renault_70_hp |
| Fuel | 40–50 octane petrol |
| Fuel System | Single carburettor |
| Cylinders | 8 |
| Cylinders Disposition | Inline |
| Bore (mm) | 96.012 |
| Stroke (mm) | 120 |
| Displacement (L) | 6.9442 |
| Compression Ratio | 4.12 |
| Valvetrain | Single overhead exhaust valve, single side inlet valve per cylinder.Although this valve arrangement is cited as "one side and one overhead valve," both valves are situated in a lateral pocket from/to… |
| Cooling | Air-cooled |
| Maximum Takeoff Power (kW) | 55.9275 |
| Specific Power (kW/L) | 0.1268 |
| Specific Fuel Consumption (g/(kW·h)) | 389.3 |