Aviation Artur Trendak: TAJFUN

General data

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Names and dates
Market original model designation
TAJFUN
Market model designation (english translation or spelling)
TAJFUN
Country of manufacture
Poland
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
560
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 diameter (option 1)
8.40
m
Main rotor diameter (option 2)
8.60
m
Main rotor diameter (option 3)
8.80
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Propeller
Mode
Pushing
Propeller direction of rotation
Counterclockwise
Powerplant
Engine model
AAT912RSCi
Engine type
Piston
Number of engines
1
Total maximum power
144
HP
Performance
Maximum horizontal flight speed (Vh)
200
km/h
Cruise speed (Vc)
170
km/h
Minimum speed
50
km/h
Take-off distance
100
m
Landing distance
5
m
Best rate of climb
7
m/s
Maximum range
1000
km
Maximum flight endurance
6
h
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