Rotax 377

377
Type Piston aero-engine
National origin Austria
Manufacturer Rotax
Major applications Ultralight 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.[1][2]

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.[1][2]

The Rotax 377 is no longer in production.[1]


Applications

Specifications (377)

Data from ROTAX 377 UL Data Sheet[1]

General characteristics

Components

Performance

See also


References

  1. ↑ 1.0 1.1 1.2 1.3 BRP-Rotax GmbH & Co. KG (n.d.). "ROTAX 377 UL - 35 HP". Retrieved 2009-03-14.
  2. ↑ 2.0 2.1 Raisner, William: LEAF catlog, 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 2009-03-14.