Kamov

Manufacturer:

Kamov

Country:

Russia

Commercial designation:

Hoodlum-A

Technical designation:

Ka-26

Version, Variant:

Type:

Contra

Currently produced:

N

Typical missions:

ALL Civil

Flight conditions:

IFR

First flight:

1965

Landing system:

wheels

Blades number:

6

Tail blades number:

0

MTOW with external loads:

3250 kg

7166.25 lbs

MTOW with only internal loading:

3076 kg

6782.58 lbs

Empty weight:

1950 kg

4299.75 lbs

External payload:

1100 kg

2425.5 lbs

Internal payload:

900 kg

1984.5 lbs

Standard fuel tank:

496 kg

1093.68 lbs

with optionnal external fuel tank:

752 kg

1658.16 lbs

Cruise speed:

100 km/h

54 kt

Maximum cruise speed:

150 km/h

81 kt

Vne:

170 km/h

91.8 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

400 km

216 nm

Max range with auxiliary external tanks:

1200 km

648 nm

Max endurance @ min consumption speed:

03:42:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

1300 m

4264 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:

800 m

2624 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:

3000 m

9840 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:

Vedeneyev

Model:

M-14V-26

Engines quantity:

2

Powerplant category:

piston

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:

239 kW

324.801 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

239 kW

324.801 hp

OEI 30s power:

120 kW

163.08 hp

OEI 2min power:

120 kW

163.08 hp

OEI max continuous power :

120 kW

163.08 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:

7.75 m

25.42 ft

Overall height:

4.05 m

13.284 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:

7

Average price:

0 $