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 edit
- Cicaré Helicopter # 1
- Cicaré CK.1
Specifications edit
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)
- Displacement: 1,307cc (79.8 in³)
- 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 4,500 rpm
- Compression ratio: 7.2:1
See also edit
Related lists
References edit
Notes edit
- ^ Taylor 1973, p. 656
Bibliography edit
- 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.