Bell Helicopter

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

Sioux

Technical designation:

47

Version, Variant:

G

Type:

Conventional

Currently produced:

N

Typical missions:

ALL

Flight conditions:

VFR

First flight:

1950

Landing system:

skids

Blades number:

2

Tail blades number:

2

MTOW with external loads:

0 kg

0 lbs

MTOW with only internal loading:

0 kg

0 lbs

Empty weight:

0 kg

0 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

128 kg

282.24 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

169 km/h

91.26 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

0 km

0 nm

Max range with auxiliary external tanks:

0 km

0 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:

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:

Franklin

Model:

6V350-B

Engines quantity:

1

Powerplant category:

piston

Main rotor rotation speed:

350 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:

173 kW

235.107 hp

Transmission shaft max continuous power:

173 kW

235.107 hp

Transmission shaft max power:

173 kW

235.107 hp

Takeoff power 5 min:

173 kW

235.107 hp

OEI 30s power:

173 kW

235.107 hp

OEI 2min power:

173 kW

235.107 hp

OEI max continuous power :

173 kW

235.107 hp

OEI max continuous transmission power:

173 kW

235.107 hp

OEI 30 sec transmission power:

173 kW

235.107 hp

OEI 2 min transmission power:

173 kW

235.107 hp

Overall length:

13.17 m

43.1976 ft

Rotor diameter:

11.31 m

37.0968 ft

Tail rotor diameter:

1.78 m

5.8384 ft

Fuselage length:

9.9 m

32.472 ft

Overall height:

2.82 m

9.2496 ft

Main rotor blades chord:

0.28 m

0.9184 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:

1

Max pax number:

2

Average price:

0 $