Solo 2625
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]
| Solo 2625 | |
|---|---|
| Type | Aircraft engine |
| National origin | Germany |
| Manufacturer | Solo Vertriebs- und Entwicklungs GmbH |
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)
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 01". aircraft.solo.global. Retrieved 13 April 2018.
- Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 02". aircraft.solo.global. Retrieved 13 April 2018.
- Solo Vertriebs- und Entwicklungs GmbH. "Solo Aircraft Engine 2625 02i". aircraft.solo.global. Retrieved 13 April 2018.
External links
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.