Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 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
      460 m2
    • Main rotor diameter
      12 m
      19 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
      2 m
      4 m
    • Empty weight
      2753 kg
      4131 kg
    • Max. takeoff weight (Gross weight)
      5443 kg
      8165 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      1407 kg
      2112 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      207 km/h
      311 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
      23 l
      320000 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
      2343 hp
      3515 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3998 m
      5999 m
    • Static ceiling
      2000 m
      3000 m
    • Range (Ferry range)
      380 km
      570 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      336 km
      504 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
      1 m/min
      36000 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Bell 214

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
14.6
88.7
Height (m)
0.6
 
3.9
50.1
Rotors
Main rotor diameter (m)
1.2
 
15.2
62
Tail rotor diameter (m)
0.8
 
3.0
4.9
Weights
Empty weight (kg)
8
 
3,441.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,803.9
575,000
Capacity
Crew (per.)
1
 
2
112
Payload (kg)
23
 
1,759.9
122,470
Capacity passengers (per.)
1
 
14
400
Speeds
Сruise Speed (km/h)
52
 
259
3,087
Power
Total Power (hp)
0.4
 
2,929.0
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,998.7
161,544
Static ceiling (m)
3
 
2,500
5,485
Range (Ferry range) (km)
4
 
475
40,700
Сombat radius (km)
277
 
420
7,210
Stat
Introduction 1974
First flight 1970

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