Parma Mikron III UL
From Wikipedia, the free encyclopedia
| Mikron III UL | |
|---|---|
| Type | Aircraft engine |
| National origin | Czech Republic |
| Manufacturer | Parma Technik sro |
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]
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
- Fuel type: gasoline
- Cooling system: air
- Reduction gear: none
Performance
- Power output: 75 hp (56 kW)