Marcmotor ROS200 explained
The
Marcmotor ROS200 is an Italian
aircraft engine, designed and produced by Marcmotor of
Macerata for use in
ultralight aircraft.
[1] Design and development
The ROS200 is a twin-cylinder two-stroke, in-line, 1961NaN1 displacement, fan-forced air-cooled, petrol engine design, with a helical gear mechanical gearbox reduction drive with a reduction ratio of 3.5:1. It employs a single capacitor discharge ignition and produces 400NaN0 at 9000 rpm, with a compression ratio of 10.6.[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.
