Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      5 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
      1 m2
      2 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
      73 kg/m2
    • Tail rotor diameter
      1 m
      2 m
    • Empty weight
      1268 kg
      1904 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1996 kg
      2994 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      192 km/h
      288 km/h
    • Сruise Speed
      140 km/h
      212 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
      363 l
      545 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
      520 hp
      780 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3660 m
      5490 m
    • Static ceiling
      2928 m
      4392 m
    • Range (Ferry range)
      208 km
      312 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      3 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
      393 m/min
      591 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      3 qt
      5 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      2 kg
    • Number built
      1760 qt
      2640 qt
    • Price
      3920000 USD
      5880000 USD

Bell 406

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
12.9
88.7
Height (m)
0.6
 
3.9
50.1
Rotors
Disc area (m2)
1.4
 
1.4
460
Main rotor diameter (m)
1.2
 
10.7
62
Tail rotor diameter (m)
0.8
 
1.7
4.9
Weights
Empty weight (kg)
8
 
1,586
276,800
Loaded weight (kg)
5
 
2,495
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
240
28,165
Сruise Speed (km/h)
52
 
176
3,087
Fuel
Fuel Capacity (l)
23
 
454
320,000
Power
Total Power (hp)
0.4
 
650
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,575
161,544
Static ceiling (m)
3
 
3,660
5,485
Range (Ferry range) (km)
4
 
260
40,700
Endurance (h)
0.0
 
2
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
492
36,000
Combat
Guns (qt)
1
 
1
18
M3P .50 cal (12.7mm) machine gun
Missiles (qt)
1
 
4
24
2 x AGM-114 Hellfire missiles and 2 x JAGM (Joint Air-to-Ground Missile)
Rockets weight (kg)
1
 
1
48
M260 rocket launcher w/ seven 2.75" Hydra 70 rockets
Stat
Number built (qt)
0
 
2,200
43,000
Price (USD)
41.5
 
4.9 million
750.0 million
Introduction 1983
First flight 10.01.1966

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