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    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      49 m2
    • Wingspan (Beam)
      12 m
      20 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
      1 m
      62 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
      0 m
      5 m
    • Empty weight
      5118 kg
      7678 kg
    • Max. takeoff weight (Gross weight)
      9979 kg
      14969 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
      672 km/h
      1008 km/h
    • Сruise Speed
      568 km/h
      852 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      28 kN
      44 kN
    • Service ceiling
      11200 m
      16800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2640 km
      3960 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
      1377 m/min
      2067 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      9 min
      14 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 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 40

TypeAircraft
Company

Bell Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
13.7
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
40.0
925
Wingspan (Beam) (m)
0.1
 
16.2
95
Weights
Empty weight (kg)
8
 
6,397.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,473.8
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
840
28,165
at 4775 m
Сruise Speed (km/h)
52
 
710
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
36
1,914
2 powerplants 18 kN each
Performance
Service ceiling (m)
0.6
 
14,000
161,544
Range (Ferry range) (km)
4
 
2,785
40,700
Internal fuel
4
 
3,300
40,700
With drop tanks
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,722.1
36,000
Time to altitude (min)
0.6
 
11.5
105
to 9100 m
Combat
Guns (qt)
1
 
6
18
6 × .50 in (12.7 mm) M2 machine guns or .60 in (15.2 mm) T17E3 machine guns (prototypes) or
1
 
4
18
20 mm (0.79 in) Hispano cannons or
1
 
1
18
37 mm (1.46 in) cannon in the nose
Stat
Introduction 1945
First flight 25.02.1945

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