Simonini Mini 2 Evo
The Simonini Mini 2 Evo is an Italian aircraft engine, designed and produced by Simonini Racing of San Dalmazio di Serramazzoni for use in ultralight aircraft.[1]
| Mini 2 Evo | |
|---|---|
| Type | Aircraft engine |
| National origin | Italy |
| Manufacturer | Simonini Racing |
Design and development
The Mini 2 Evo is a single cylinder two-stroke, air-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratios of 2.3:1 or 3.0:1. It employs capacitor discharge ignition and produces 33 hp (25 kW) at 8000 rpm.[1]
Applications
Specifications (Mini 2 Evo)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Single cylinder, two stroke aircraft engine
- Bore: 70 mm (2.8 in)
- Stroke: 60 mm (2.4 in)
- Displacement: 231 cc (14.1 cu in)
- Length: 260 mm (10.2 in)
- Width: 330 mm (13.0 in)
- Height: 428 mm (16.9 in)
- Dry weight: 19.3 kg (42.5 lb)
Components
- Fuel type: gasoline
- Cooling system: air
- Reduction gear: Poly V belt
Performance
- Power output: 33 hp (25 kW) at 8000 rpm
- Compression ratio: 10:1
References
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
External links
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.