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    • Year
      1906
      2018
    • Length
      23 m
      35 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      148 m2
      223 m2
    • Wingspan (Beam)
      34 m
      52 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      7
      12
    • 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
      26028 kg
      39042 kg
    • Max. takeoff weight (Gross weight)
      40000 kg
      60000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      85 per.
      129 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      312 km/h
      468 km/h
    • Сruise Speed
      268 km/h
      404 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
      7680 hp
      11520 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1832 km
      2748 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
      278 m/min
      418 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
      16 qt
      24 qt
    • Price
      41 USD
      750000000 USD

Breguet 761 Deux-Ponts

TypeAircraft
Company

Breguet Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
28.9
88.7
Height (m)
0.6
 
9.6
50.1
Wings
Wing area (m2)
1.1
 
185.4
925
Wingspan (Beam) (m)
0.1
 
43.0
95
Aspect ratio
1.7
 
10.0
25.6
Weights
Empty weight (kg)
8
 
32,535
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
50,000
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
107
400
Speeds
Max. Speed (km/h)
25
 
390
28,165
at 3000 m
Сruise Speed (km/h)
52
 
336
3,087
Power
Total Power (hp)
0.4
 
9,600
60,000
4 powerplants 2400 hp each
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Range (Ferry range) (km)
4
 
2,290
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
348
36,000
at sea level
Stat
Number built (qt)
0
 
20
43,000
Introduction 1949
First flight 15.02.1949
Stop production 31.03.1971

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