Parma Mikron III UL explained
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] Design and development
The Mikron III UL is a four-cylinder four-stroke, in-line, 24401NaN1 displacement, air-cooled, direct-drive, gasoline engine design. It employs dual magnetos and produces 750NaN0 at 2760 rpm, with a compression ratio of 7.0:1.[1]
Notes and References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015.
