ОКБ М. Л. Миля: Ми-60 МАИ
Mil: Mi-60 MAI

General data

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Names and dates
Market original model designation
Ми-60
Market model designation (english translation or spelling)
Mi-60
Original model name
МАИ
Model name (english translation or spelling)
MAI
Project start date
1993
Mockup construction date
2001
Country of manufacture
Russia
People involved
N. Tishchenko {Н. Тищенко}Project leader
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
1400
kg
Manufacturers empty weight (MEW)
1000
kg
Cabin and cockpit
Maximum number of passengers onboard
2
Maximum number of people onboard
3
Main rotor
Main rotor type
Bearingless
Main rotor diameter
10
m
Number of blades
3
Tail rotor
Tail rotor type
Classic tail rotor
Tail rotor diameter
1.13
m
Number of blades
2
Powerplant
Engine model
Lom-Praga M-334A
Engine type
Piston
Number of engines
2
Total maximum power
280
HP
Performance
Maximum horizontal flight speed (Vh)
210
km/h
Cruise speed (Vc)
190
km/h
Best rate of climb
8
m/s
Maximum service ceiling
4500
m
Hover ceiling OGE
2000
m
Maximum range
400
km
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