Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      91 m2
    • Wingspan (Beam)
      13 m
      21 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
      1012 kg
      1518 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1760 kg
      2640 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
      128 km/h
      192 km/h
    • Сruise Speed
      112 km/h
      168 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
      360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 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
      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
      73 m/min
      111 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      440 kg
      660 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      160 qt
      240 qt
    • Price
      41 USD
      750000000 USD

Breguet 16

TypeAircraft
Company

Breguet Aviation

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
75.5
925
Wingspan (Beam) (m)
0.1
 
17.0
95
Weights
Empty weight (kg)
8
 
1,265
276,800
Loaded weight (kg)
5
 
2,200
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
160
28,165
Сruise Speed (km/h)
52
 
140
3,087
Power
Total Power (hp)
0.4
 
300
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Range (Ferry range) (km)
4
 
900
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
92
36,000
Combat
Guns (qt)
1
 
1
18
trainable 7.7 mm (.303 in) Lewis Gun in observer's cockpit
Bombs weight (kg)
2
 
550
39,000
Stat
Number built (qt)
0
 
200
43,000
Introduction 1918
First flight 01.06.1918
Stop production 1926

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