Cicaré: CH-9
Cicare: CH-9

General data

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Names and dates
Market original model designation
CH-9
Market model designation (english translation or spelling)
CH-9
First flight date and time
1995
Country of manufacture
Argentina
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
390
kg
Manufacturers empty weight (MEW)
160
kg
External dimensions
Total length (rotors turning)
7.30
m
Main rotor
Main rotor diameter
6.10
m
Number of blades
2
Tail rotor
Tail rotor diameter
1.10
m
Number of blades
2
Powerplant
Engine model
Rotax 447
Engine type
Piston
Number of engines
2
Total maximum continuous power
90
HP
Performance
Never exceed speed (Vne)
165
km/h
Cruise speed (Vc)
115
km/h
Best rate of climb
7.50
m/s
Maximum service ceiling
3500
m
Maximum range
290
km
Maximum flight endurance
2.50
h
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