| Aircraft Engine Manufacturer |
Bristol Engine Company (Bristol) |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
874.9797 |
| Diameter (mm) |
139.7 |
| Length (mm) |
135.001 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Bristol_Hercules |
| Fuel |
87 Octane petrol |
| Fuel System |
Claudel-Hobson carburettor |
| Cylinders |
14 |
| Cylinders Disposition |
radial |
| Bore (mm) |
146.05 |
| Stroke (mm) |
165 |
| Displacement (L) |
38.6735 |
| Supercharger |
Single-speed centrifugal type supercharger |
| Compression Ratio |
7 |
| Valvetrain |
Gear-driven sleeve valves with five ports per sleeve — three intake and two exhaust |
| Cooling |
Air-cooled |
| Maximum Takeoff Power (kW) |
948.5302 |
| Specific Power (kW/L) |
0.425 |
| Power To Weight (kW/kg) |
0.7 |
| Specific Fuel Consumption (g/(kW·h)) |
261.6 |