ХАИ: ХАИ-32
KhAI: HAI-32

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
ХАИ-32
Market model designation (english translation or spelling)
HAI-32
Project start date
1978
Date of prototype completion
1979
Tests start date
1979
Country of manufacture
Ukraine
People involved
S. Ryabikov {С. Рябиков}Chief design engineer
K. Vasilenko {К. Василенко}Design engineer
P. Dimitrov {П. Ди­митров}Design engineer
V. Podimai {В. Подымай}Design engineer
A. Babahanov {А. Бабаханов}Design engineer
Victor Manuylenko {Виктор Мануйленко}Design engineer
A. Podgornyi {А. Подгорный}Design engineer
A. Fefelov {А. Фефелов}Design engineer
Fursa Grigorievitch {Фурса Григорьевич}Project supervisor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
220
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Length
3.25
m
Width
1.80
m
Height
1.95
m
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.20
m
Number of blades
2
Propeller
Mode
Pushing
Propeller direction of rotation
Clockwise
Propeller pitch mode
Constant pitch
Number of blades
2
Propeller material
Wood
Powerplant
Engine model
Dnepr {Днепр} MT-9
Number of engines
1
Total maximum power
40
HP
Performance
Maximum horizontal flight speed (Vh)
90
km/h
Cruise speed (Vc)
65
km/h
Take-off speed
37
km/h
Landing speed
25
km/h
Miminum rate of descend in autorotation
4.50
m/s
0.1045