Kamov

Manufacturer:

Kamov

Country:

Russia

Commercial designation:

Alligator

Technical designation:

Ka-52

Version, Variant:

Type:

Contra

Currently produced:

Y

Typical missions:

Military Combat Attack

Flight conditions:

First flight:

2013

Landing system:

wheels

Blades number:

6

Tail blades number:

0

MTOW with external loads:

10400 kg

22932 lbs

MTOW with only internal loading:

10800 kg

23814 lbs

Empty weight:

0 kg

0 lbs

External payload:

2000 kg

4410 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

1484 kg

3272.22 lbs

with optionnal external fuel tank:

3204 kg

7064.82 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

260 km/h

140.4 kt

Vne:

300 km/h

162 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

3.5 g

Range with normal tanks:

460 km

248.4 nm

Max range with auxiliary external tanks:

1100 km

594 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

12 m/s

2361.6 ft/min

Rate of climb @ SL @MTOW:

8 m/s

1574.4 ft/min

IGE max hovering altitude, MTOW:

0 m

0 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

3900 m

12792 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

5500 m

18040 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Y

Engine manufacturer:

Motor Sich

Model:

VK-2500

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0.286 kg/kW/h

0.46904 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

2574 kW

3498.066 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

3528 kW

4794.552 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

1985 kW

2697.615 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

16 m

52.48 ft

Rotor diameter:

14.5 m

47.56 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

13.465 m

44.1652 ft

Overall height:

4.93 m

16.1704 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

2

Max pax number:

0

Average price:

15000000 $