Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      273 kg/m2
      411 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
      4800 kg
      7200 kg
    • Max. takeoff weight (Gross weight)
      8600 kg
      12901 kg
    • Loaded weight
      7360 kg
      11040 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
      872 km/h
      1308 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
      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
      27 kN
      41 kN
    • Service ceiling
      11411 m
      17118 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2600 km
      3900 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
      1867 m/min
      2802 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      3 qt
      5 qt
    • Rockets
      4 qt
      8 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1120 kg
      1680 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      299 qt
      449 qt
    • Price
      41 USD
      750000000 USD

North American Aviation FJ-4 Fury

TypeAircraft
Company

North American Aviation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wingspan (Beam) (m)
0.1
 
11.9
95
Wing loading (kg/m2)
3.1
 
341.7
829
Weights
Empty weight (kg)
8
 
6,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,750.1
575,000
Loaded weight (kg)
5
 
9,200
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,090
28,165
at 10670 m
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
34
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
14,264.6
161,544
Range (Ferry range) (km)
4
 
3,250
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,334.8
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.787 in) cannon
Missiles (qt)
1
 
4
24
AIM-9 Sidewinder missiles
Rockets (qt)
1
 
6
76
LAU-3/A 70mm rocket pods
Bombs weight (kg)
2
 
1,400
39,000
of underwing ordnance, including missiles
Stat
Number built (qt)
0
 
374
43,000
First flight 28.10.1954
Stop production 01.12.1960

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