Aviation Artur Trendak: TERCEL

General data

Producer info

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Names and dates
Market original model designation
TERCEL
Market model designation (english translation or spelling)
TERCEL
Country of manufacture
Poland
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
560
kg
Manufacturers empty weight (MEW)
350
kg
(...)
285
kg
Cabin and cockpit
Maximum number of people onboard
2
Cabin width
1.25
m
External dimensions
Length
4.90
m
Width
2.20
m
Height
2.80
m
Main landing gear wheel diameter
0.35
m
Nose landing gear wheel diameter
0.35
m
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
Prerotation type
Mechanical
Number of blades
2
Propeller
Mode
Pushing
Propeller diameter
1.74
m
Propeller direction of rotation
Counterclockwise
Thrust
2746
N
Powerplant
Engine model
CA 912 ULT (RST)
Engine type
Piston
Number of engines
1
Total maximum power
135
HP
(...)
122
HP
Fuel system
Fuel tank capacity
120
l
Performance
Never exceed speed (Vne)
210
km/h
Maximum horizontal flight speed (Vh)
175
km/h
Cruise speed (Vc)
140
km/h
Minimum speed
50
km/h
Take-off distance
100
m
Landing distance
15
m
(...)
5
m
0
m
Best rate of climb
6.10
m/s
Maximum service ceiling
4500
m
Maximum range
800
km
Maximum flight endurance
6
h
0.0589