ХАИ: ХАИ-22А
KhAI: HAI-22A

General data

Producer info

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Names and dates
Market original model designation
ХАИ-22А
Market model designation (english translation or spelling)
HAI-22A
Date of prototype completion
1968
Country of manufacture
Ukraine
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
220
kg
Manufacturers empty weight (MEW)
131
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Nose landing gear wheel diameter
0.32
m
Main rotor
Main rotor diameter
5.40
m
Number of blades
2
Tail rotor
Tail rotor diameter
1.10
m
Number of blades
2
Powerplant
Engine model
М-62
Engine model (english translation or spelling)
M-62
Engine type
Piston
Number of engines
1
Total maximum power
36
HP
Performance
Maximum horizontal flight speed (Vh)
100
km/h
Cruise speed (Vc)
70
km/h
Maximum service ceiling
1000
m
Maximum range
200
km
0.0893