Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      5 m
      8 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
      2299 kg
      3449 kg
    • Max. takeoff weight (Gross weight)
      3621 kg
      5433 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
      920 km/h
      1380 km/h
    • Сruise Speed
      772 km/h
      1158 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
      17 kN
      27 kN
    • Service ceiling
      12167 m
      18252 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      965 km
      1449 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
      1 m/min
      36000 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Bell X-5

TypeAircraft
Company

Bell Aircraft Corporation

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
16.3
925
Wingspan (Beam) (m)
0.1
 
10.2
95
Unswept
0.1
 
6.5
95
60° sweep
Weights
Empty weight (kg)
8
 
2,874.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,526.9
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,150
28,165
Сruise Speed (km/h)
52
 
965
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Thrust (kN)
1.5
 
21.8
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
15,209.5
161,544
Range (Ferry range) (km)
4
 
1,207
40,700
Stat
Number built (qt)
0
 
2
43,000
Introduction 1951
First flight 20.06.1951
Stop production 01.12.1958

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