| Zenoah G-25 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Zenoah |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 23.1332 |
| Length (mm) | 29.9974 |
| Height (mm) | 37.6936 |
| Width (mm) | 29.3878 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Zenoah_G-25 |
| Fuel | unleaded auto fuel |
| Oil System | pre-mixed |
| Bore (mm) | 72 |
| Stroke (mm) | 60 |
| Displacement (L) | 0.242 |
| Compression Ratio | 6.5 |
| Valvetrain | piston ported |
| Cooling | free air |
| Maximum Takeoff Power (kW) | 16.4054 |