Simonini Mini 4

Mini 4
Type Aircraft engine
National origin Italy
Manufacturer Simonini Racing




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, gasoline 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

Components

Performance

See also


Related lists

References

  1. 1 2 3 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 - version of the Tuesday, June 23, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.