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    • Year
      1906
      2018
    • Length
      13 m
      21 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
      1 m2
      460 m2
    • Main rotor diameter
      11 m
      17 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
      2463 kg
      3696 kg
    • Max. takeoff weight (Gross weight)
      4318 kg
      6478 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      2400 kg
      3600 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      10 per.
      16 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      207 km/h
      311 km/h
    • Сruise Speed
      184 km/h
      276 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
      1248 l
      1872 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
      1440 hp
      2160 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4876 m
      7316 m
    • Static ceiling
      2632 m
      3948 m
    • Range (Ferry range)
      784 km
      1176 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
      695 qt
      1043 qt
    • Price
      41 USD
      750000000 USD

Bell 412

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
17.1
88.7
Height (m)
0.6
 
4.6
50.1
Rotors
Main rotor diameter (m)
1.2
 
14.0
62
Tail rotor diameter (m)
0.8
 
2.6
4.9
Weights
Empty weight (kg)
8
 
3,079.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,397.8
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
3,000
90,700
Capacity passengers (per.)
1
 
13
400
Speeds
Max. Speed (km/h)
25
 
259
28,165
Сruise Speed (km/h)
52
 
230
3,087
Fuel
Fuel Capacity (l)
23
 
1,560
320,000
Power
Total Power (hp)
0.4
 
1,800
60,000
2 powerplants 900 hp each
Performance
Service ceiling (m)
0.6
 
6,096
161,544
Static ceiling (m)
3
 
3,290
5,485
Range (Ferry range) (km)
4
 
980
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
411.5
36,000
Stat
Number built (qt)
0
 
869
43,000
Introduction 1979

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