Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 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
      64 m2
      98 m2
    • Main rotor diameter
      8 m
      13 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      22 kg/m2
    • Tail rotor diameter
      1 m
      2 m
    • Empty weight
      845 kg
      1269 kg
    • Max. takeoff weight (Gross weight)
      1161 kg
      1742 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
      3 per.
      5 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      192 km/h
      290 km/h
    • Сruise Speed
      172 km/h
      260 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
      275 l
      413 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
      332 hp
      499 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3291 m
      4938 m
    • Static ceiling
      3120 m
      4680 m
    • Range (Ferry range)
      554 km
      832 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
      329 m/min
      494 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
      5840 qt
      8760 qt
    • Price
      720000 USD
      1080000 USD

Bell 206

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
12.1
88.7
Height (m)
0.6
 
2.8
50.1
Rotors
Disc area (m2)
1.4
 
81.1
460
Main rotor diameter (m)
1.2
 
10.2
62
Disc loading (kg/m2)
17.1
 
18.1
73
Tail rotor diameter (m)
0.8
 
1.7
4.9
Weights
Empty weight (kg)
8
 
1,057.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,451.5
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
4
400
Speeds
Max. Speed (km/h)
25
 
241
28,165
Сruise Speed (km/h)
52
 
216
3,087
Fuel
Fuel Capacity (l)
23
 
344
320,000
Power
Total Power (hp)
0.4
 
415.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,114.8
161,544
Static ceiling (m)
3
 
3,900
5,485
Range (Ferry range) (km)
4
 
692.7
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
411.5
36,000
Stat
Number built (qt)
0
 
7,300
43,000
Price (USD)
41.5
 
900,000
750.0 million
Introduction 1966
First flight 08.12.1962

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