- Cicaré 4C2T
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Cicaré 4C2T Type Air-cooled four-cylinder horizontally opposed two-stroke piston engine National origin Argentina Manufacturer Cicaré Aeronáutica First run 1973 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.
Contents
Application
- Cicaré Helicopter # 1
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
- Power output: 69 hp (67 kW) at 4,5000 rpm
- Compression ratio: 7.2:1
See also
- Related lists
References
Notes
- ^ Taylor 1973, p. 656
Bibliography
- Jane's All the World's Aircraft 1973-74. London, United Kingdom: Jane's Yearbooks. 1973. ISBN 0 354 00117 5.
Lists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- Aircraft piston engines 1970-1979
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