Top Qs
Timeline
Chat
Perspective
Simonini Mini 4
Italian aircraft engine From Wikipedia, the free encyclopedia
Remove ads
The Simonini Mini 4 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 4 is a single cylinder two-stroke, air-cooled, petrol engine design, with a poly V belt reduction drive with reduction ratios of 2.56:1 and 2.78:1. It employs capacitor discharge ignition electronic ignition and produces 20 hp (15 kW) at 7200 rpm.[1]
Specifications (Mini 4)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Single Twin cylinder, two stroke aircraft engine
- Bore: 61 mm (2.4 in)
- Stroke: 54 mm (2.1 in)
- Displacement: 160 cc (9.8 cu in)
- Length: 300 mm (11.8 in)
- Width: 400 mm (15.7 in)
- Height: 200 mm (7.9 in)
- Dry weight: 11 kg (24.3 lb)
Components
- Fuel type: petrol
- Cooling system: air
- Reduction gear: poly V belt reduction drive, reduction ratios of 2.56:1 and 2.78:1
Performance
- Power output: 20 hp (15 kW) at 7200 rpm
- Compression ratio: 10:1
Remove ads
See also
Related lists
References
External links
Wikiwand - on
Seamless Wikipedia browsing. On steroids.
Remove ads