Search filter

    • Year
      1906
      2018
    • Length
      25 m
      38 m
    • Height
      8 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      145 m2
    • Wingspan (Beam)
      29 m
      45 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
      20560 kg
      30840 kg
    • Max. takeoff weight (Gross weight)
      36960 kg
      55440 kg
    • Loaded weight
      36000 kg
      54000 kg
    • Crew
      9 per.
      15 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      9 per.
      15 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      518 km/h
      778 km/h
    • Сruise Speed
      252 km/h
      378 km/h
    • Stall Speed
      133 km/h
      201 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
      18500 l
      27750 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
      9760 hp
      14640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7316 m
      10974 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7260 km
      10890 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      14 h
      22 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
      705 m/min
      1059 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
      2800 kg
      4200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      69 qt
      105 qt
    • Price
      28000000 USD
      42000000 USD

Breguet 1150 Atlantic

TypeAircraft
Company

Breguet Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
31.6
88.7
Height (m)
0.6
 
10.9
50.1
Wings
Wing area (m2)
1.1
 
120.3
925
Wingspan (Beam) (m)
0.1
 
37.4
95
Weights
Empty weight (kg)
8
 
25,700
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
46,200
575,000
Loaded weight (kg)
5
 
45,000
242,500
Capacity
Crew (per.)
1
 
12
112
Capacity passengers (per.)
1
 
12
400
12 passengers or relief crew
Speeds
Max. Speed (km/h)
25
 
648
28,165
Сruise Speed (km/h)
52
 
315
3,087
Stall Speed (km/h)
40
 
167
257.7
flaps down
Fuel
Fuel Capacity (l)
23
 
23,125
320,000
Power
Total Power (hp)
0.4
 
12,200
60,000
2 powerplants 6100 hp each
Performance
Service ceiling (m)
0.6
 
9,145
161,544
Range (Ferry range) (km)
4
 
9,075
40,700
Endurance (h)
0.0
 
18
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
882
36,000
Combat
Bombs weight (kg)
2
 
3,500
39,000
including torpedoes, depth charges, mines, anti-ship missiles, bombs and/or buoys
Stat
Number built (qt)
0
 
87
43,000
Price (USD)
41.5
 
35.0 million
750.0 million
Introduction 1961
First flight 21.10.1961

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