Cicaré CH-4

from Wikipedia, the free encyclopedia
Cicaré CH-4
f2
Type: helicopter
Design country:

ArgentinaArgentina Argentina

Manufacturer:

Cicaré Helicópteros

First flight:

1982

Number of pieces:

1

The Cicaré CH-4 was a helicopter made by the Argentine manufacturer Cicaré Helicópteros .

history

In 1982 Augusto Cicaré developed the CH-4, one of the world's first ultralight helicopters. He made sure to keep the costs as low as possible and only used local materials. The helicopter had excellent maneuverability and was extremely stable in flight. The CH-4 served as the basis for a number of other helicopter developments by Cicaré.

construction

The CH-4 was a single-seat, ultralight helicopter of conventional design, powered by a two-cylinder two-stroke boxer engine with 40.5 kW, which Augusto Cicaré converted from a motorcycle engine. The motor drives the two-bladed main rotor and the tail rotor. The helicopter actually consists of a few steel tubes welded together, onto which an engine and a seat are mounted. Of course, the helicopter had the necessary controls and landing skids.

Technical specifications

Parameter Data
crew 1
length 7.53 m
height 1.6 m
Rotor diameter 6 m
Empty mass 135 kg
Max. Takeoff mass 270 kg
Cruising speed 100 km / h
Top speed 130 km / h
Service ceiling 2100 m
Range 200 km
Engines 1 × two-cylinder two-stroke boxer engine with 40.5 kW

See also

Web links

Individual evidence

  1. Data from cicare.com.ar , accessed June 30, 2016