The Sodemo V2-1.0 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1]
| V2-1.0 | |
|---|---|
| Type | Aircraft engine |
| National origin | France |
| Manufacturer | Sodemo |
Design and development edit
The engine is a 90° V-twin-cylinder four-stroke, 992 cc (60.5 cu in) displacement, liquid-cooled, petrol engine design, with a mechanical gearbox reduction drive. It employs dual capacitor discharge ignition and produces 102 hp (76 kW) at 6500 rpm.[1]
Specifications (V2-1.0) edit
Data from Tacke[1]
General characteristics
- Type: Twin cylinder, four stroke aircraft engine
- Bore: 90 mm (3.5 in)
- Stroke: 78 mm (3.1 in)
- Displacement: 992 cc (60.5 cu in)
- Dry weight: 55 kg (121.3 lb)
Components
- Fuel type: petrol
- Cooling system: liquid
Performance
- Power output: 102 hp (76 kW)
See also edit
Related development
Related lists