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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      28 m
      42 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
      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
      1115 kg
      1674 kg
    • Max. takeoff weight (Gross weight)
      1995 kg
      2994 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
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      222 km/h
      334 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
      275 l
      413 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
      672 hp
      1008 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2438 m
      3658 m
    • Static ceiling
      3120 m
      4680 m
    • Range (Ferry range)
      583 km
      876 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
      487 m/min
      732 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Bell 400

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wingspan (Beam) (m)
0.1
 
35
95
Rotors
Main rotor diameter (m)
1.2
 
10.6
62
Tail rotor diameter (m)
0.8
 
1.7
4.9
Weights
Empty weight (kg)
8
 
1,394.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,494.8
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
278
28,165
Сruise Speed (km/h)
52
 
259
3,087
Fuel
Fuel Capacity (l)
23
 
344
320,000
Power
Total Power (hp)
0.4
 
840
60,000
2 powerplants 420 hp each
Performance
Service ceiling (m)
0.6
 
3,048
161,544
Static ceiling (m)
3
 
3,900
5,485
Range (Ferry range) (km)
4
 
729.7
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
609.6
36,000
Stat
Number built (qt)
0
 
4
43,000
Introduction 1984
First flight 04.04.1984

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