Kamov

Manufacturer:

Kamov

Country:

Russia

Commercial designation:

Black Shark

Technical designation:

Ka-50

Version, Variant:

Type:

Contra

Currently produced:

N

Typical missions:

Military Combat Attack

Flight conditions:

First flight:

1982

Landing system:

wheels

Blades number:

6

Tail blades number:

0

MTOW with external loads:

10800 kg

23814 lbs

MTOW with only internal loading:

10800 kg

23814 lbs

Empty weight:

7800 kg

17199 lbs

External payload:

3000 kg

6615 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

1440 kg

3175.2 lbs

with optionnal external fuel tank:

3040 kg

6703.2 lbs

Cruise speed:

270 km/h

145.8 kt

Maximum cruise speed:

300 km/h

162 kt

Vne:

389 km/h

210.06 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

3.5 g

Range with normal tanks:

518 km

279.72 nm

Max range with auxiliary external tanks:

1100 km

594 nm

Max endurance @ min consumption speed:

01:40:00 h:min

Rate of climb @ SL:

10 m/s

1968 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 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:

4000 m

13120 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:

TV3-117VMA

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 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:

3266 kW

4438.494 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 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:

14.2 m

46.576 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:

1

Max pax number:

0

Average price:

0 $