Simonini Victor 2
| Victor 2 | |
|---|---|
| Type | Aircraft engine |
| National origin | Italy |
| Manufacturer | Simonini Racing |
|
| |
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]
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
References
External links
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