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.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015.
Design and development The engine series are all twin-cylinder two-stroke, in-line, displacement, liquid-cooled, gasoline engine designs, with poly V belt reduction drives. They employ dual electronic ignition ignitions systems and produce , depending on the model, with a compression ratio of 9.5:1.
Variants Solo 2625 01 Model with a single diaphragm carburetor, that produces at 5,900 rpm. Solo 2625 02 Model with dual diaphragm carburetors, that produces at 6,500 rpm. Solo 2625 02i Model with fuel injection, that produces at 6,600 rpm.
Applications Binder EB28 Binder EB29 Glaser-Dirks DG-500 Glaser-Dirks DG-800 HpH 304 Rolladen-Schneider LS9 Schempp-Hirth Arcus Schempp-Hirth Quintus Schempp-Hirth Ventus-2 Sportinė Aviacija LAK-20
Specifications (2625 02i)
See also
References
External links