Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      38 m2
      57 m2
    • Wingspan (Beam)
      11 m
      18 m
    • Wing loading
      25 kg/m2
      39 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
      808 kg
      1212 kg
    • Max. takeoff weight (Gross weight)
      1228 kg
      1844 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      152 km/h
      228 km/h
    • Сruise Speed
      121 km/h
      183 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
      240 hp
      361 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      720 km
      1080 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      3 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
      233 m/min
      351 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
      240 kg
      360 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      6240 qt
      9360 qt
    • Price
      41 USD
      750000000 USD

Breguet 14

TypeAircraft
Company

Breguet Aviation

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.9
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
47.5
925
Wingspan (Beam) (m)
0.1
 
14.4
95
Wing loading (kg/m2)
3.1
 
32
829
at max. takeoff weight
Weights
Empty weight (kg)
8
 
1,010
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,536
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
190
28,165
Сruise Speed (km/h)
52
 
152
3,087
Power
Total Power (hp)
0.4
 
300.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Range (Ferry range) (km)
4
 
900
40,700
Endurance (h)
0.0
 
2.5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
292
36,000
Combat
Guns (qt)
1
 
3
18
1 × fixed 7.7 mm (.303 in) Vickers machine gun; 2 × flexible 7.7 mm (.303 in) Lewis Gun for observer
Bombs weight (kg)
2
 
300
39,000
Stat
Number built (qt)
0
 
7,800
43,000
Introduction 1916
First flight 21.11.1916

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