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    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      2 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
      10 m
      16 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
      1646 kg
      2470 kg
    • Max. takeoff weight (Gross weight)
      2993 kg
      4491 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.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      231 km/h
      347 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
      571 l
      857 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
      1088 hp
      1632 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3852 m
      5778 m
    • Static ceiling
      1732 m
      2598 m
    • Range (Ferry range)
      720 km
      1080 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
      409 m/min
      615 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
      177 qt
      267 qt
    • Price
      41 USD
      750000000 USD

Bell 222

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
15.4
88.7
Height (m)
0.6
 
3.7
50.1
3,56 - 3,71 m depending on variant
Rotors
Main rotor diameter (m)
1.2
 
12.8
62
Tail rotor diameter (m)
0.8
 
2.1
4.9
Weights
Empty weight (kg)
8
 
2,058
276,800
2066 - 2312 kg
Max. takeoff weight (Gross weight) (kg)
154
 
3,742
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
289
28,165
Сruise Speed (km/h)
52
 
259
3,087
Fuel
Fuel Capacity (l)
23
 
714
320,000
Power
Total Power (hp)
0.4
 
1,360
60,000
2 powerplants 618-700hp each depending on variant
Performance
Service ceiling (m)
0.6
 
4,815
161,544
3901 0 4815 m depending on variant
Static ceiling (m)
3
 
2,165
5,485
Range (Ferry range) (km)
4
 
900
40,700
600 - 900 km depending on variant
Dynamic Performance
Rate of climb (m/min)
1.9
 
512
36,000
Stat
Number built (qt)
0
 
222
43,000
Introduction 1976
First flight 13.08.1976

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