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Solo 2625

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The Solo 2625 is a series of German aircraft engines, designed and produced by Solo Vertriebs- und Entwicklungs GmbH of Fellbach for use in ultralight aircraft, self-launching sailplanes and homebuilt aircraft.[1]

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Design and development

The engine series are all twin-cylinder two-stroke, in-line, 625 cc (38.1 cu in) displacement, liquid-cooled, gasoline engine designs, with poly V belt reduction drives. They employ dual electronic ignition ignitions systems and produce 53 to 68 hp (40 to 51 kW), depending on the model, with a compression ratio of 9.5:1.[1]

Variants

Solo 2625 01
Model with a single diaphragm carburetor, that produces 53 hp (40 kW) at 5,900 rpm.[2]
Solo 2625 02
Model with dual diaphragm carburetors, that produces 64 hp (48 kW) at 6,500 rpm.[3]
Solo 2625 02i
Model with fuel injection, that produces 68 hp (51 kW) at 6,600 rpm.[1][4]

Applications

Specifications (2625 02i)

Data from Tacke[1]

General characteristics

  • Type: Twin cylinder, two stroke aircraft engine
  • Bore: 76 mm (3.0 in)
  • Stroke: 69 mm (2.7 in)
  • Displacement: 625 cc (38.1 cu in)
  • Dry weight: 24 kg (52.9 lb)

Components

  • Fuel type: gasoline
  • Cooling system: liquid
  • Reduction gear: poly V belt

Performance

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See also

Related lists

References

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