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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      80 m2
      121 m2
    • Main rotor diameter
      9 m
      14 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      1 m
      3 m
    • Empty weight
      686 kg
      1031 kg
    • Max. takeoff weight (Gross weight)
      1070 kg
      1606 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      135 km/h
      203 km/h
    • Сruise Speed
      114 km/h
      172 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      172 l
      260 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      224 hp
      336 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2732 m
      4098 m
    • Static ceiling
      1876 m
      2814 m
    • Range (Ferry range)
      317 km
      476 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      209 m/min
      315 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      4480 qt
      6720 qt
    • Price
      41 USD
      750000000 USD

Bell 47

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
2.8
50.1
Rotors
Disc area (m2)
1.4
 
100.8
460
Main rotor diameter (m)
1.2
 
11.3
62
Tail rotor diameter (m)
0.8
 
1.8
4.9
Weights
Empty weight (kg)
8
 
858.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,338.1
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
169
28,165
Сruise Speed (km/h)
52
 
143
3,087
Fuel
Fuel Capacity (l)
23
 
216
320,000
Power
Total Power (hp)
0.4
 
280
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,415
161,544
Static ceiling (m)
3
 
2,345
5,485
Range (Ferry range) (km)
4
 
396.3
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
262.1
36,000
Stat
Number built (qt)
0
 
5,600
43,000
Introduction 1960
First flight 08.12.1945

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