Simonini Victor 1 Super
| Victor 1 Super | |
|---|---|
| Type | Aircraft engine |
| National origin | Italy |
| Manufacturer | Simonini Racing |
|
| |
The Simonini Victor 1 Super 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 1 Super is a single cylinder two-stroke, liquid-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratios of 2.70:1, 2.80:1 and 3.00:1. It employs dual capacitor discharge ignition electronic ignition and produces 54 hp (40 kW) at 6200 rpm.[1]
Specifications (Victor 1 Super)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Single cylinder, two stroke aircraft engine
- Bore: 80 mm (3.1 in)
- Stroke: 76 mm (3.0 in)
- Displacement: 401 cc (24.5 cu in)
- Length: 320 mm (12.6 in)
- Width: 340 mm (13.4 in)
- Height: 350 mm (13.8 in)
- Dry weight: 32 kg (70.5 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid
- Reduction gear: poly V belt reduction drive, reduction ratios of 2.70:1, 2.80:1 and 3.00:1
Performance
- Power output: 54 hp (40 kW) at 6200 rpm
- Compression ratio: 9.5:1
See also
- Related lists
References
External links
This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.