Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      35 m
      53 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
      10 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
      2394 kg
      3593 kg
    • Max. takeoff weight (Gross weight)
      3628 kg
      5444 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      221 km/h
      333 km/h
    • Сruise Speed
      52 km/h
      3087 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
      252 km/h
      378 km/h
    • Fuel Capacity
      784 l
      1176 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
      2974 m
      4463 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      405 km
      609 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
      395 m/min
      593 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      6 qt
      10 qt
    • Rockets
      5 qt
      9 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      892 qt
      1340 qt
    • Price
      9040000 USD
      13560000 USD

Bell AH-1 Cobra

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
16.1
88.7
with both rotors turning
Height (m)
0.6
 
4.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
44
95
Rotors
Main rotor diameter (m)
1.2
 
13.4
62
Tail rotor diameter (m)
0.8
 
2.6
4.9
Weights
Empty weight (kg)
8
 
2,993.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,535.9
575,000
Capacity
Crew (per.)
1
 
2
112
one pilot, one co-pilot/gunner
Speeds
Max. Speed (km/h)
25
 
277
28,165
Never exceed speed (km/h)
108.0
 
315
1,050
Fuel
Fuel Capacity (l)
23
 
980
320,000
Power
Total Power (hp)
0.4
 
1,800
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,718.6
161,544
Range (Ferry range) (km)
4
 
507.5
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
493.8
36,000
Combat
Guns (qt)
1
 
1
18
General Dynamics 20 mm (0.787 in) M197 3-barreled Gatling cannon
Missiles (qt)
1
 
8
24
missiles mounted in two-missile launchers on each hardpoint
Rockets (qt)
1
 
7
76
mounted in the M260 launcher
Stat
Number built (qt)
0
 
1,116
43,000
Price (USD)
41.5
 
11.3 million
750.0 million
Introduction 1967
First flight 07.09.1965

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