Search filter

    • Year
      1906
      2018
    • Length
      8 m
      12 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      139 kg/m2
      209 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
      2480 kg
      3720 kg
    • Max. takeoff weight (Gross weight)
      3920 kg
      5880 kg
    • Loaded weight
      3200 kg
      4800 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
      411 km/h
      617 km/h
    • Max. Speed
      528 km/h
      792 km/h
    • Сruise Speed
      486 km/h
      730 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1440 hp
      2160 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10485 m
      15728 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      580 km
      870 km
    • Range PTB (Ferry range)
      2832 km
      4248 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
      609 m/min
      915 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
      4 qt
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      544 kg
      816 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2642 qt
      3964 qt
    • Price
      52731 USD
      79097 USD

Bell P-63 Kingcobra

TypeAircraft
Company

Bell Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
23
925
Wingspan (Beam) (m)
0.1
 
11.7
95
Wing loading (kg/m2)
3.1
 
173.9
829
Weights
Empty weight (kg)
8
 
3,100
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,900
575,000
Loaded weight (kg)
5
 
4,000
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
514
1,500
Max. Speed (km/h)
25
 
660
28,165
at 7620 m
Сruise Speed (km/h)
52
 
608
3,087
Power
Total Power (hp)
0.4
 
1,800
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
13,106.4
161,544
Range (Ferry range) (km)
4
 
725
40,700
Range PTB (Ferry range) (km)
720
 
3,540
10,000
Dynamic Performance
Rate of climb (m/min)
1.9
 
762
36,000
Combat
Guns (qt)
1
 
5
18
1 x 37 mm M4 cannon; 4× 0.50 in (12.7mm) M2 Browning machine guns (two synchronized in the nose, two in the wings)
Bombs weight (kg)
2
 
680
39,000
bomb load on wing and fuselage
Stat
Number built (qt)
0
 
3,303
43,000
Price (USD)
41.5
 
65,914
750.0 million
Introduction 1942
First flight 07.12.1942

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