Mitsubishi

Manufacturer:

Mitsubishi

Country:

Japan

Commercial designation:

MH2000

Technical designation:

MH2000

Version, Variant:

Type:

Fenestron

Currently produced:

N

Typical missions:

Civil

Flight conditions:

VFR

First flight:

1996

Landing system:

skids

Blades number:

4

Tail blades number:

10

MTOW with external loads:

4500 kg

9922.5 lbs

MTOW with only internal loading:

4500 kg

9922.5 lbs

Empty weight:

2500 kg

5512.5 lbs

External payload:

0 kg

0 lbs

Internal payload:

2000 kg

4410 lbs

Standard fuel tank:

912 kg

2010.96 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

250 km/h

135 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

278 km/h

150.12 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

777 km

419.58 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:00:00 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:

2700 m

8856 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:

0 m

0 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:

Mitsubishi

Model:

Mitsubishi MG5-1 10

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:

1306 kW

1774.854 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

1306 kW

1774.854 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:

14 m

45.92 ft

Rotor diameter:

12.2 m

40.016 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

12.2 m

40.016 ft

Overall height:

3.8 m

12.464 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:

12

Average price:

0 $