Вертолёты России: Ка-62
Russian Helicopters: Ka-62

General data

Producer info

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Names and dates
Market original model designation
Ка-62
Market model designation (english translation or spelling)
Ka-62
First flight date and time
2016-04-28
Country of manufacture
Russia
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
6500
kg
Cabin and cockpit
Maximum number of people onboard
17
External dimensions
Length
13.50
m
Width
2.76
m
Height
4.87
m
Main rotor
Main rotor diameter
13.80
m
Number of blades
5
Tail rotor
Tail rotor type
Fenestron
Powerplant
Engine model
Turbomeca Ardiden 3G
Engine type
Turboshaft
Number of engines
2
Total maximum continuous power
3090
HP
Total maximum power
3550
HP
(...)
3552
HP
Emergency power (single engine)
1941
HP
(...)
1940
HP
Performance
Never exceed speed (Vne)
310
km/h
Maximum horizontal flight speed (Vh)
290
km/h
(...)
308
km/h
Cruise speed (Vc)
240
km/h
(...)
290
km/h
Best rate of climb
14
m/s
Maximum service ceiling
6100
m
(...)
5700
m
Hover ceiling IGE
3800
m
Hover ceiling OGE
3200
m
(...)
3300
m
Maximum range
720
km
(...)
770
km
Maximum flight endurance
4
h
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