Cicaré 4C2T

The Cicaré 4CT2 is an Argentine air-cooled, four-cylinder, horizontally opposed, two-stroke, piston engine designed and built by Cicaré Aeronáutica as a light, low cost engine.

Cicaré 4C2T
Type Air-cooled four-cylinder horizontally opposed two-stroke piston engine
National origin Argentina
Manufacturer Cicaré Aeronáutica
First run 1973

Application

Specifications

Data from Jane's All the World's Aircraft 1994-95[1]

General characteristics

  • Type: Air-cooled four-cylinder horizontally opposed two-stroke piston engine
  • Bore: 74 mm (2.91 in)
  • Stroke: 76 mm (3.00 in)
  • Length: 810 mm (31.89 in)
  • Width: 660 mm (25.98 in)
  • Height: 550 mm (21.65 in)
  • Dry weight: 68 kg (150 lb)

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cylinder
  • Fuel system: Updraught flow-type carburettor
  • Fuel type: Mixture of 40 parts 80-octane to 1 part SAE40 oil
  • Cooling system: Air-cooled

Performance

See also

Related lists

References

Notes

  1. Taylor 1973, p. 656

Bibliography

  • Taylor, John W.R., ed. (1973). Jane's All the World's Aircraft 1973-74. London, United Kingdom: Jane's Yearbooks. ISBN 0-354-00117-5.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.