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Cicaré 4C2T

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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
  • Cicaré CK.1

    • Specifications

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

    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

    • References

    Cicaré 4C2T Wikipedia
    (Text) CC BY-SA