Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      9 m
      15 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 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
      870 km/h
      1306 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      687 km/h
      1031 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
      0 hp
      60000 hp
    • Thrust
      21 kN
      33 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1274 km
      1912 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
      1868 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
      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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

North American Aviation FJ-2/-3 Fury

TypeAircraft
Company

North American Aviation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.5
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
26.7
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
1,088
1,500
Сruise Speed (km/h)
52
 
859
3,087
Power
Thrust (kN)
1.5
 
26.7
1,914
1 powerplant
Performance
Range (Ferry range) (km)
4
 
1,593
40,700
narmal
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,335
36,000
Stat
Introduction 1951

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