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The Simonini Victor 2 is an Italian aircraft engine, designed and produced by Simonini Racing of San Dalmazio di Serramazzoni for use in ultralight aircraft.[1]

Victor 2
Type	Aircraft engine
National origin	Italy
Manufacturer	Simonini Racing

Design and development

The Victor 2 is a twin cylinder, in-line, two-stroke, liquid-cooled, gasoline engine design, with a mechanical gearbox reduction drive with reduction ratios of 2.54:1 to 4.00:1. It employs dual capacitor discharge ignition and produces 92 hp (69 kW) at 6200 rpm.[1]

Specifications (Victor 2)

Data from World Directory of Leisure Aviation 2011-12[1]

General characteristics

• Type: Twin cylinder, two stroke aircraft engine
• Bore: 80 mm (3.1 in)
• Stroke: 72 mm (2.8 in)
• Displacement: 724 cc (44.2 cu in)
• Length: 648 mm (25.5 in)
• Width: 410 mm (16.1 in)
• Height: 490 mm (19.3 in)
• Dry weight: 52 kg (114.6 lb)

Components

• Fuel type: gasoline
• Cooling system: liquid
• Reduction gear: a mechanical gearbox reduction drive, reduction ratios of 2.54:1 to 4.00:1

Performance

• Power output: 92 hp (69 kW) at 6200 rpm
• Compression ratio: 9.5:1

See also

Related lists

• List of aircraft engines

References

External links

• Official website

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