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.
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==
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==