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Austrian two-stroke aircraft engine From Wikipedia, the free encyclopedia
The Rotax 377 is a 35 hp (26 kW), twin-cylinder, two-stroke aircraft engine, that was built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.[1][2]
377 | |
---|---|
Type | Piston aero-engine |
National origin | Austria |
Manufacturer | Rotax |
Major applications | Ultralight aircraft |
The Rotax 377 features piston-ported, air-cooled cylinder heads and cylinders, utilizing either a fan or free air for cooling. Lubrication is by use of pre-mixed fuel and oil. The 377 has a single Bosch Flywheel Magneto Generator 12 volt ignition system and is equipped with a 36 mm Bing double float carburetor, with either a hand lever or cable choke.[1][2]
The Rotax 377 is no longer in production.[1]
Data from ROTAX 377 UL Data Sheet[1]
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