Cicaré CH-9
| Cicaré CH-9 | |
|---|---|
| Type: | helicopter |
| Design country: | |
| Manufacturer: | |
| First flight: |
1995 |
| Number of pieces: |
1 |
The Cicaré CH-9 was a helicopter made by the Argentine manufacturer Cicaré Helicópteros .
History and construction
The single-seat CH-9 was a further development of the Cicaré CH-7 . Its frame was made of welded steel tubes and had no cabin. It was powered by two Rotax 447 two - cylinder two-stroke engines with 33 kW each and had a main rotor made of composite materials.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| length | 7.30 m |
| height | 1.80 m |
| Rotor diameter | 6.10 m |
| Empty mass | 160 kg |
| Max. Takeoff mass | 390 kg |
| Cruising speed | 115 km / h |
| Top speed | 165 km / h |
| Service ceiling | 3500 m |
| Range | 290 km |
| Engines | 2 × Rotax 447 two - cylinder two-stroke engines with 33 kW each |
See also
Web links
- CH-9 at cicare.com.ar , accessed February 17, 2016
- La visita a Cicaré Helicópteros SA (Spanish), accessed February 17, 2016
Individual evidence
- ↑ Data from cicare.com.ar , accessed on February 17, 2016