Search filter

    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      51 m2
      78 m2
    • Wingspan (Beam)
      19 m
      29 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
      8360 kg
      12540 kg
    • Max. takeoff weight (Gross weight)
      11600 kg
      17400 kg
    • Loaded weight
      11600 kg
      17400 kg
    • Crew
      2 per.
      4 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
      448 km/h
      672 km/h
    • Сruise Speed
      423 km/h
      635 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
      4320 hp
      6480 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1215 km
      1823 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Breguet 482

TypeAircraft
Company

Breguet Aviation

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
18.9
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wing area (m2)
1.1
 
64.4
925
Wingspan (Beam) (m)
0.1
 
24.1
95
Weights
Empty weight (kg)
8
 
10,450
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,500
575,000
Loaded weight (kg)
5
 
14,500
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
560
28,165
at 8000 m
Сruise Speed (km/h)
52
 
529
3,087
Power
Total Power (hp)
0.4
 
5,400
60,000
4 powerplants 1350 hp each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
1,519
40,700
Stat
Introduction 1947
First flight 27.11.1947

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