Mil

Manufacturer:

Mil

Country:

Russia

Commercial designation:

Euromil prototype

Technical designation:

Mi-38

Version, Variant:

Type:

Conventional

Currently produced:

N

Typical missions:

Civil Firefight Utility Rescue Transport Offshore

Flight conditions:

First flight:

2003

Landing system:

wheels

Blades number:

6

Tail blades number:

4

MTOW with external loads:

16200 kg

35721 lbs

MTOW with only internal loading:

15600 kg

34398 lbs

Empty weight:

0 kg

0 lbs

External payload:

7000 kg

15435 lbs

Internal payload:

5000 kg

11025 lbs

Standard fuel tank:

3055 kg

6736.275 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

295 km/h

159.3 kt

Vne:

320 km/h

172.8 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

920 km

496.8 nm

Max range with auxiliary external tanks:

1300 km

702 nm

Max endurance @ min consumption speed:

00:00:00 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:

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:

0 m

0 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:

50 °C

90 °F

Lowest use Temperature:

-60 °C

-108 °F

APU in HC:

Engine manufacturer:

Pratt & Whitney

Model:

PW-127T/S

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:

3728.5 kW

5067.0315 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:

0 m

0 ft

Rotor diameter:

21 m

68.88 ft

Tail rotor diameter:

3.84 m

12.5952 ft

Fuselage length:

20.15 m

66.092 ft

Overall height:

0 m

0 ft

Main rotor blades chord:

6.98 m

22.8944 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:

30

Average price:

0 $