Kamov

Manufacturer:

Kamov

Country:

Russia

Commercial designation:

Hoodlum-B

Technical designation:

Ka-126

Version, Variant:

Type:

Contra

Currently produced:

N

Typical missions:

ALL Civil

Flight conditions:

IFR

First flight:

1986

Landing system:

wheels

Blades number:

6

Tail blades number:

0

MTOW with external loads:

3250 kg

7166.25 lbs

MTOW with only internal loading:

3250 kg

7166.25 lbs

Empty weight:

1915 kg

4222.575 lbs

External payload:

1000 kg

2205 lbs

Internal payload:

1335 kg

2943.675 lbs

Standard fuel tank:

640 kg

1411.2 lbs

with optionnal external fuel tank:

896 kg

1975.68 lbs

Cruise speed:

160 km/h

86.4 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

180 km/h

97.2 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

713 km

385.02 nm

Max range with auxiliary external tanks:

1015 km

548.1 nm

Max endurance @ min consumption speed:

05:36:00 h:min

Rate of climb @ SL:

6.6 m/s

1298.88 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

970 m

3181.6 ft

IGE max hovering altitude, empty:

0 m

0 ft

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

100 m

328 ft

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

0 m

0 ft

OGE max hovering altitude, MTOW:

80 m

262.4 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:

3850 m

12628 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:

Engine manufacturer:

Omsk Engine Design Bureau

Model:

Mars TV-O-100

Engines quantity:

1

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:

522 kW

709.398 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:

13 m

42.64 ft

Rotor diameter:

13 m

42.64 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

7.78 m

25.5184 ft

Overall height:

4.16 m

13.6448 ft

Main rotor blades chord:

0.25 m

0.82 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:

8

Average price:

0 $