Rotax 377

377
TypePiston aero-engine
National originAustria
ManufacturerRotax
Major applicationsUltralight aircraft

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.

Development

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.

The Rotax 377 is no longer in production.

Applications

Specifications (377)

Data from ROTAX 377 UL Data Sheet

General characteristics

Components

Performance

See also

References

  1. 1 2 3 4 BRP-Rotax GmbH & Co. KG (n.d.). "ROTAX 377 UL - 35 HP" (PDF). Retrieved 14 March 2009.
  2. 1 2 Raisner, William: LEAF catalog, pages 6-105. Leading Edge Airfoils, 1995.
  3. ↑ Civil Aviation Authority (United Kingdom) (1995). "CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)". Retrieved 14 March 2009.