Mil

Manufacturer:

Mil

Country:

Russia

Commercial designation:

Hind-F

Technical designation:

Mi-35

Version, Variant:

P

Type:

Conventional

Currently produced:

Y

Typical missions:

Military Combat Attack

Flight conditions:

First flight:

1974

Landing system:

wheels

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:

8620 kg

19007.1 lbs

External payload:

2400 kg

5292 lbs

Internal payload:

2400 kg

5292 lbs

Standard fuel tank:

1640 kg

3616.2 lbs

with optionnal external fuel tank:

3240 kg

7144.2 lbs

Cruise speed:

217 km/h

117.18 kt

Maximum cruise speed:

280 km/h

151.2 kt

Vne:

320 km/h

172.8 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

450 km

243 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:

12.5 m/s

2460 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:

1750 m

5740 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:

4500 m

14760 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:

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:

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:

3275 kW

4450.725 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:

21.35 m

70.028 ft

Rotor diameter:

17.3 m

56.744 ft

Tail rotor diameter:

3.91 m

12.8248 ft

Fuselage length:

17.51 m

57.4328 ft

Overall height:

5 m

16.4 ft

Main rotor blades chord:

0.58 m

1.9024 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:

3

Max pax number:

8

Average price:

0 $