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, 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

Performance

See also

Related lists

References

  1. ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X