Cicaré CH-11
Cicaré CH-11 | |
---|---|
Type: | helicopter |
Design country: | |
Manufacturer: | |
First flight: |
1998 |
The Cicaré CH-11 is a helicopter made by the Argentine manufacturer Cicaré Helicópteros .
History and construction
The CH-11 is a further development of the Cicaré CH-10 and, like this one, has coaxial rotors which, like the closed cabin, are made of composite materials. The single-seat cabin can be entered through side doors, whereby a hood that can be opened as a whole is also available. The helicopter itself consists of welded steel tubes and is powered by a Rotax 912 four-cylinder four-stroke boxer engine with 75 kW. It would also be possible to install a different motor. Due to its small size, the CH-11 is very manoeuvrable. A variant of the CH-11 is the CH-11C , which can be used both manned and unmanned.
The Argentine military is evaluating the CH-11C for use as a UAV.
Versions
- CH-10 - the standard model
- CH-10C - the model that can be used both manned and unmanned
Technical specifications
Parameter | Data |
---|---|
crew | 1 |
length | 3.96 m |
height | 2.06 m |
Rotor diameter | 4.2 m |
Empty mass | 150 kg |
Max. Takeoff mass | 270 kg |
Cruising speed | 110 km / h |
Top speed | 135 km / h |
Service ceiling | 2100 m |
Range | 210 km |
Engines | 1 × Rotax-912 - four-cylinder , four-stroke boxer engine with 75 kW |
See also
Web links
- CH-11 at cicare.com.ar , accessed February 18, 2016
- CH-11 on avia.pro , accessed on February 18, 2017
Individual evidence
- ↑ a b Data on avia.pro , accessed on February 18, 2017