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Simonini Mini 3
Italian aircraft engine From Wikipedia, the free encyclopedia
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The 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]
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
- AEF Monotrace
- Sperwill 3+
- Rev UL Trike
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
Performance
- Power output: 33 hp (25 kW) at 7000 rpm
- Compression ratio: 10.5:1
See also
Related lists
References
External links
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