Apollo: Gyro AG1

General data

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Names and dates
Market original model designation
Gyro AG1
Market model designation (english translation or spelling)
Gyro AG1
Country of manufacture
Hungary
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
500
kg
Manufacturers empty weight (MEW)
256
kg
Cabin and cockpit
Maximum number of people onboard
2
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Collective control
No
Main rotor diameter
8.40
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Propeller
Mode
Pushing
Propeller direction of rotation
Counterclockwise
Number of blades
3
Powerplant
Engine model (option 1)
Rotax 912 ULS
Engine model (option 2)
Rotax 914 UL
Fuel system
Fuel tank capacity
50
l
Performance
Never exceed speed (Vne)
180
km/h
Maximum horizontal flight speed (Vh)
160
km/h
Cruise speed (Vc)
120
km/h
Minimum speed
30
km/h
Take-off distance
70
m
(...)
10
m
Landing distance
15
m
(...)
0
m
Best rate of climb
5
m/s
0.0984