Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      72 m2
    • Wingspan (Beam)
      16 m
      25 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
      3368 kg
      5052 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6560 kg
      9840 kg
    • Crew
      4 per.
      6 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
      320 km/h
      480 km/h
    • Сruise Speed
      256 km/h
      384 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
      1286 hp
      1930 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8000 m
      12000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1600 km
      2400 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      860 kg
      1292 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Breguet 460

TypeAircraft
Company

Breguet Aviation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
60
925
Wingspan (Beam) (m)
0.1
 
20.6
95
Weights
Empty weight (kg)
8
 
4,210
276,800
Loaded weight (kg)
5
 
8,200
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
400
28,165
Сruise Speed (km/h)
52
 
320
3,087
Power
Total Power (hp)
0.4
 
1,608
60,000
2 powerplants 804 hp each
Performance
Service ceiling (m)
0.6
 
10,000
161,544
Range (Ferry range) (km)
4
 
2,000
40,700
Combat
Guns (qt)
1
 
3
18
1 × fixed, forward-firing 20 mm Hispano-Suiza HS.404 cannon; 2 × rearward-firing machine guns
Bombs weight (kg)
2
 
1,076
39,000
Stat
Introduction 1935
First flight 1935

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