Solo 2625

Solo 2625
TypeAircraft engine
National originGermany
ManufacturerSolo Vertriebs- und Entwicklungs GmbH

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

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.

Variants

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

Applications

Specifications (2625 02i)

Data from Tacke

General characteristics

Components

Performance

See also

Related lists

References

  1. 1 2 3 4 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ↑ Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 01". aircraft.solo.global. Retrieved 13 April 2018.
  3. ↑ Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 02". aircraft.solo.global. Retrieved 13 April 2018.
  4. ↑ Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 02i". aircraft.solo.global. Retrieved 13 April 2018.