avia.wikisort.org - EngineThe Simonini Mini 3 is an Italian aircraft engine, designed and produced by Simonini Racing of San Dalmazio di Serramazzoni for use in ultralight aircraft.[1]
Italian aircraft engine
Design and development
The Mini 3 is a single cylinder twin cylinder two-stroke, air liquid-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratios of 2.49:1, 2.57:1 and 2.76:1. It employs electronic ignition and produces 33 hp (25 kW) at 7000 rpm.[1]
Applications
Specifications (Mini 3)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Single cylinder, two stroke aircraft engine
- Bore: 73 mm (2.9 in)
- Stroke: 65 mm (2.6 in)
- Displacement: 270 cc (16.5 cu in)
- Length: 256 mm (10.1 in)
- Width: 375 mm (14.8 in)
- Height: 498 mm (19.6 in)
- Dry weight: 20 kg (44.1 lb)
Components
- Fuel type: gasoline
- Cooling system: air
- Reduction gear: poly V belt reduction drive, reduction ratios of 2.49:1, 2.57:1 and 2.76:1
- Power output: 33 hp (25 kW) at 7000 rpm
- Compression ratio: 10.5:1
See also
Related lists
References
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
External links
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