Parma Mikron III UL

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]

Mikron III UL
Type Aircraft engine
National origin Czech Republic
Manufacturer Parma Technik sro

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)
gollark: It doesn't wipe.
gollark: Fewer eggs about maybe? Hard to say.
gollark: Using my patented ***ALGORITHM*** of basic statistics and wild guessing™.
gollark: That's basically what I said (the extra volume of halloween stuff mucks up the ratios).
gollark: Any opinions on my theory of what's going on with the pricing? Basically, I said that if extra dragons are introduced to the total but not the rest of the system (golds, whatever else), then rarer stuff's ratios will be affected more than common stuff, so the gold pricing goes crazy and nebulae stay the same.

See also

Related development

Related lists

References

  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
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.