ARGO.Aero: Xenon IV Executive

General data

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Names and dates
Market original model designation
Xenon IV Executive
Market model designation (english translation or spelling)
Xenon IV Executive
Country of manufacture
Poland
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
560
kg
Manufacturers empty weight (MEW)
295
kg
Cabin and cockpit
Maximum number of people onboard
2
Control system
Lateral control
Main rotor
Longitudinal control
Main rotor
Yaw control
Rudder
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Collective control
No
Main rotor direction of rotation
Counterclockwise
Prerotation type
Mechanical
Max main rotor angular speed in prerotation
250
rpm
Number of blades
2
Propeller
Mode
Pushing
Propeller direction of rotation
Counterclockwise
Powerplant
Engine model
CA 912 ULS-T
Total maximum power
135
HP
Fuel system
Fuel tank capacity
84
l
Performance
Maximum horizontal flight speed (Vh)
195
km/h
Cruise speed (Vc)
160
km/h
Take-off distance
100
m
(...)
50
m
Landing distance
5
m
(...)
0
m
Best rate of climb
6.1
m/s
Maximum service ceiling
5486
m
Maximum range
640
km
0.0514