Моисеенко В. З.: Мо-1
Moiseenko V. Z.: Mo-1

General data

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Names and dates
Market original model designation
Мо-1
Market model designation (english translation or spelling)
Mo-1
Date of prototype completion
1984
Country of manufacture
Ukraine
People involved
Valery Moiseenko {Валерий Моисеенко}Constructor
E. Frolov {Е. Фролов}Test pilot
Config info
Rotorcraft typeAutogyro
Weights
Manufacturers empty weight (MEW)
85
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Main landing gear wheel diameter
0.28
m
Main landing gear wheel width
0.08
m
Nose landing gear wheel diameter
0.26
m
Nose landing gear wheel width
0.09
m
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Collective control
No
Main rotor diameter
6.10
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Propeller
Mode
Pushing
Propeller direction of rotation
Counterclockwise
Number of blades
2
Propeller material
Metal
Thrust
588
N
Powerplant
Engine type
Piston
Number of engines
1
Total maximum power
42
HP
0.0763