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    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 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
      85 m2
      129 m2
    • Main rotor diameter
      12 m
      20 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
      3440 kg
      5161 kg
    • Max. takeoff weight (Gross weight)
      6350 kg
      9526 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      2904 kg
      4356 kg
    • Payload
      2904 kg
      4356 kg
    • Capacity passengers
      13 per.
      21 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      211 km/h
      317 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
      1648 l
      2472 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
      2600 hp
      3900 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2535 m
      3804 m
    • Static ceiling
      1168 m
      1752 m
    • Range (Ferry range)
      686 km
      1030 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
      434 m/min
      652 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
      76 qt
      116 qt
    • Price
      41 USD
      750000000 USD

Bell 214ST

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
15.0
88.7
Height (m)
0.6
 
4.8
50.1
Rotors
Disc area (m2)
1.4
 
107.3
460
Main rotor diameter (m)
1.2
 
15.9
62
Tail rotor diameter (m)
0.8
 
3.0
4.9
Weights
Empty weight (kg)
8
 
4,300.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,937.9
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
3,630
90,700
Payload (kg)
23
 
3,630
122,470
Capacity passengers (per.)
1
 
17
400
Speeds
Max. Speed (km/h)
25
 
264
28,165
Сruise Speed (km/h)
52
 
259
3,087
Fuel
Fuel Capacity (l)
23
 
2,060
320,000
Power
Total Power (hp)
0.4
 
3,250
60,000
2 powerplants 1625 hp each
Performance
Service ceiling (m)
0.6
 
3,169.9
161,544
Static ceiling (m)
3
 
1,460
5,485
Range (Ferry range) (km)
4
 
858
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
542.5
36,000
Stat
Number built (qt)
0
 
96
43,000
Introduction 1977
First flight 01.02.1977

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