Parma_Mikron_III_UL

Parma Mikron III UL

Parma Mikron III UL

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The Parma Mikron III UL is a Czech aircraft engine, developed from the Walter Mikron and produced by Parma Technik sro of Luhačovice for use in ultralight aircraft.[1]

Quick Facts Mikron III UL, Type ...

Design and development

The Mikron III UL is a four-cylinder four-stroke, in-line, 2,440 cc (148.9 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs dual magnetos and produces 75 hp (56 kW) at 2760 rpm, with a compression ratio of 7.0:1.[1]

Specifications (Mikron III UL)

Data from Tacke[1]

General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 90 mm (3.5 in)
  • Stroke: 96 mm (3.8 in)
  • Displacement: 2,440 cc (148.9 cu in)
  • Dry weight: 72 kg (158.7 lb)

Components

Performance

  • Power output: 75 hp (56 kW)

See also

Related development

Related lists

References

  1. [1]
    Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
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