avia.wikisort.org - Helicopter

The Cicaré CH-2 was a helicopter designed and built by Augusto Cicaré in Argentina in the early 1960s.

CH-2
Role	General-use helicopter Type of aircraft
Manufacturer	Cicaré
Designer	Augusto Cicaré
First flight	1964
Number built	1

Design

The CH-2 was a two-seat, single-engine helicopter whose airframe and tail boom was made from steel. The main rotor 3 three blades, and the tail rotor transmission was carried out through a shaft. The main transmission featured a 90° stage and belts stage.[1][2]

Specifications

Data from Augusto Cicare Helicopters CH.2 tech data[3]

General characteristics

• Crew: one
• Capacity: one passenger
• Length: 8.45 m (27 ft 9 in)
• Width: 1.80 m (5 ft 11 in)
• Height: 2.35 m (7 ft 9 in)
• Empty weight: 390 kg (860 lb)
• Max takeoff weight: 690 kg (1,521 lb)
• Powerplant: 1 × Lycoming O-360 4-cylinder air-cooled horizontally-opposed piston engine, 135 kW (181 hp)
• Main rotor diameter: 7.30 m (23 ft 11 in)

Performance

• Maximum speed: 165 km/h (103 mph, 89 kn)
• Cruise speed: 135 km/h (84 mph, 73 kn)
• Service ceiling: 3,200 m (10,500 ft)

References

На других языках

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[de] Cicaré CH-2

Die Cicaré CH-2 war ein Hubschrauber des argentinischen Herstellers Cicaré Helicópteros.

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- [en] Cicaré CH-2

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