Walter Mikron
The Walter Mikron is a four-cylinder, aircooled, inverted straight engine for powering light aircraft. First run in 1938 in Czechoslovakia, it is still in production. With a displacement of 2.4 L (149 cu in), it produces 48 kW (65 hp) at 2,600 rpm.[1]. Since 1999, the engine is produced by Parma Technik, in Luhačovice[2].
Applications
Specifications (Mikron)
General characteristics
- Type: 4-cylinder inverted air-cooled inline
- Bore: 85 mm (3.35 in)
- Stroke: 96 mm (3.78 in)
- Displacement: 2.44 L (149 cu in)
- Length: 804 mm (31.65 in)
- Width: 341 mm (13.46 in)
- Height: 635 mm (25.0 in)
- Dry weight: 60 kg (132 lb)
Components
- Valvetrain: One intake and one exhaust valve per cylinder
- Fuel system: 1 Claudel carburettor
- Fuel type: 68 octane
- Cooling system: Air-cooled
Performance
See also
- Comparable engines
- Related lists
References
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
External links
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