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Sodemo V2-1.0

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V2-1.0
Type Aircraft engine
National origin France
Manufacturer Sodemo

The Sodemo V2-1.0 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1]

Design and development

The engine is a 90° V-twin-cylinder four-stroke, 992 cc (60.5 cu in) displacement, liquid-cooled, gasoline 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)

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: gasoline
  • Cooling system: liquid

Performance

  • Power output: 102 hp (76 kW)

See also

Related development

Related lists

References

  1. ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015. ISSN 1368-485X
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