Cicaré: CH-4
Cicare: CH-4

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
CH-4
Market model designation (english translation or spelling)
CH-4
First flight date and time
1982
Country of manufacture
Argentina
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
270
kg
Manufacturers empty weight (MEW)
135
kg
External dimensions
Total length (rotors turning)
7.53
m
Main rotor
Main rotor diameter
6
m
Number of blades
2
Tail rotor
Tail rotor diameter
1.10
m
Powerplant
Engine model
Cicare 2 Cyl boxer
Engine type
Piston
Number of engines
1
Total maximum continuous power
55
HP
Performance
Never exceed speed (Vne)
130
km/h
Cruise speed (Vc)
100
km/h
Best rate of climb
6
m/s
Maximum service ceiling
2100
m
Maximum range
200
km
Maximum flight endurance
2
h
0.0879