Cicaré: CH-1
Cicare: CH-1

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
CH-1
Market model designation (english translation or spelling)
CH-1
First flight date and time
1961
Country of manufacture
Argentina
Config info
Rotorcraft typeHelicopter
Config
Coaxial rotors
Weights
Maximum Takeoff Weight (MTOW)
330
kg
Manufacturers empty weight (MEW)
225
kg
External dimensions
Total length (rotors turning)
6.80
m
Overal height
2.15
m
Main rotor
Main rotor diameter
6
m
Number of blades
2
Powerplant
Engine model
Cicare 1.8
Engine type
Piston
Number of engines
1
Total maximum continuous power
60
HP
Performance
Never exceed speed (Vne)
120
km/h
Cruise speed (Vc)
90
km/h
Best rate of climb
7
m/s
Maximum service ceiling
1500
m
0.0432