Mil

Manufacturer:

Mil

Country:

Russia

Commercial designation:

Hind-E

Technical designation:

Mi-35

Version, Variant:

M

Type:

Conventional

Currently produced:

Y

Typical missions:

Military Combat Attack

Flight conditions:

First flight:

0

Landing system:

Blades number:

0

Tail blades number:

0

MTOW with external loads:

12000 kg

26460 lbs

MTOW with only internal loading:

12000 kg

26460 lbs

Empty weight:

8360 kg

18433.8 lbs

External payload:

2860 kg

6306.3 lbs

Internal payload:

1500 kg

3307.5 lbs

Standard fuel tank:

1640 kg

3616.2 lbs

with optionnal external fuel tank:

3240 kg

7144.2 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

259 km/h

139.86 kt

Vne:

300 km/h

162 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

500 km

270 nm

Max range with auxiliary external tanks:

1000 km

540 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

12.4 m/s

2440.32 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:

3150 m

10332 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:

5100 m

16728 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:

Klimov

Model:

VK-2500-02

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:

0 kW

0 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

3272 kW

4446.648 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:

21.27 m

69.7656 ft

Rotor diameter:

17.2 m

56.416 ft

Tail rotor diameter:

3.84 m

12.5952 ft

Fuselage length:

17.49 m

57.3672 ft

Overall height:

5 m

16.4 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:

0

Max pax number:

0

Average price:

0 $