Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      34 m2
      52 m2
    • Wingspan (Beam)
      11 m
      18 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1472 kg
      2208 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
      174 km/h
      262 km/h
    • Сruise Speed
      149 km/h
      225 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
      360 hp
      540 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6000 m
      9000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      4 qt
      6 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
      80 qt
      120 qt
    • Price
      41 USD
      750000000 USD

Breguet 17

TypeAircraft
Company

Breguet Aviation

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
43.3
925
Wingspan (Beam) (m)
0.1
 
14.3
95
Weights
Loaded weight (kg)
5
 
1,840
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and gunner
Speeds
Max. Speed (km/h)
25
 
218
28,165
Сruise Speed (km/h)
52
 
187
3,087
Power
Total Power (hp)
0.4
 
450
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,500
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
348
36,000
Combat
Guns (qt)
1
 
5
18
2 × fixed, forward-firing 7.7 mm (.303 in) Vickers machine guns; 2 × trainable, rearward-firing 7.7 mm (.303 in) Lewis Guns in ring mount in rear cockpit; 1 × trainable, downward-firing 7.7 mm (.303 in) Lewis gun through trap door in rear cockpit
Stat
Number built (qt)
0
 
100
43,000
Introduction 1918
First flight 1918

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