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Sodemo V2-1.2

From Wikipedia, the free encyclopedia

V2-1.2
Type Aircraft engine
National origin France
Manufacturer Sodemo

The Sodemo V2-1.2 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1]

Design and development

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The engine is a 90° V-twin-cylinder four-stroke, 1,200 cc (73.2 cu in) displacement, liquid-cooled, petrol engine design, with a mechanical helical-gear gearbox reduction drive. It employs dual capacitor discharge ignition and produces 136 hp (101 kW).[1]

Specifications (V2-1.2)

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Data from Tacke[1]

General characteristics

  • Type: Twin cylinder, four stroke aircraft engine
  • Displacement: 992 cc (60.5 cu in)

Components

  • Fuel type: petrol
  • Cooling system: liquid

Performance

  • Power output: 136 hp (101 kW)

See also

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Related development

Related lists

References

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  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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