Boeing

Manufacturer:

Boeing

Country:

USA

Commercial designation:

Osprey

Technical designation:

V-22

Version, Variant:

Type:

Tilt

Currently produced:

N

Typical missions:

Military Proto

Flight conditions:

IFR

First flight:

1989

Landing system:

wheels

Blades number:

6

Tail blades number:

0

MTOW with external loads:

0 kg

0 lbs

MTOW with only internal loading:

27442 kg

60509.61 lbs

Empty weight:

14800 kg

32634 lbs

External payload:

6147 kg

13554.135 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

446 km/h

240.84 kt

Maximum cruise speed:

476 km/h

257.04 kt

Vne:

509 km/h

274.86 kt

Max negative g @ MTOW:

-1 g

Max positive g @ MTOW:

4 g

Range with normal tanks:

1759 km

949.86 nm

Max range with auxiliary external tanks:

3892 km

2101.68 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:

16.25 m/s

3198 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:

1646 m

5398.88 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:

7529 m

24695.12 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:

Y

Engine manufacturer:

Rolls-Royce

Model:

T406-AD-400

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

338 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:

9172 kW

12464.748 hp

Transmission shaft max continuous power:

6816 kW

9262.944 hp

Transmission shaft max power:

7730 kW

10505.07 hp

Takeoff power 5 min:

9172 kW

12464.748 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

5093 kW

6921.387 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:

17.48 m

57.3344 ft

Rotor diameter:

11.42 m

37.4576 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

17.48 m

57.3344 ft

Overall height:

6.74 m

22.1072 ft

Main rotor blades chord:

0.73 m

2.3944 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

97.5 °

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:

25

Average price:

0 $