Bell Helicopter

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

Venom

Technical designation:

UH-1

Version, Variant:

Y

Type:

Conventional

Currently produced:

Y

Typical missions:

Military Utility Combat

Flight conditions:

First flight:

2001

Landing system:

skids

Blades number:

4

Tail blades number:

4

MTOW with external loads:

8390 kg

18499.95 lbs

MTOW with only internal loading:

7866 kg

17344.53 lbs

Empty weight:

5369 kg

11838.645 lbs

External payload:

2250 kg

4961.25 lbs

Internal payload:

3021 kg

6661.305 lbs

Standard fuel tank:

1172 kg

2584.26 lbs

with optionnal external fuel tank:

1640 kg

3616.2 lbs

Cruise speed:

250 km/h

135 kt

Maximum cruise speed:

293 km/h

158.22 kt

Vne:

304 km/h

164.16 kt

Max negative g @ MTOW:

-0.5 g

Max positive g @ MTOW:

2.8 g

Range with normal tanks:

0 km

0 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

03:18:00 h:min

Rate of climb @ SL:

12.8 m/s

2519.04 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:

6100 m

20008 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:

General Electric

Model:

T700-GE-401C

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:

1138 kW

1546.542 hp

Transmission shaft max continuous power:

1932 kW

2625.588 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

1248 kW

1696.032 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

1346 kW

1829.214 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:

17.78 m

58.3184 ft

Rotor diameter:

14.63 m

47.9864 ft

Tail rotor diameter:

2.97 m

9.7416 ft

Fuselage length:

14.88 m

48.8064 ft

Overall height:

4.44 m

14.5632 ft

Main rotor blades chord:

0.63 m

2.0664 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:

10

Average price:

1700000 $