Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      39 m2
      60 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
      1404 kg
      2108 kg
    • Max. takeoff weight (Gross weight)
      2040 kg
      3060 kg
    • Loaded weight
      1914 kg
      2872 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
      188 km/h
      284 km/h
    • Сruise Speed
      158 km/h
      238 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6320 m
      9480 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      163 m/min
      245 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
      96 kg
      144 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      181 qt
      273 qt
    • Price
      41 USD
      750000000 USD

Breguet 27

TypeAircraft
Company

Breguet Aviation

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.8
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
49.7
925
Wingspan (Beam) (m)
0.1
 
17.0
95
Weights
Empty weight (kg)
8
 
1,756
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,550
575,000
Loaded weight (kg)
5
 
2,393
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
236
28,165
Сruise Speed (km/h)
52
 
198
3,087
Power
Total Power (hp)
0.4
 
500
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,900
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
204
36,000
Combat
Guns (qt)
1
 
3
18
1 × fixed, forward-firing 7.7 mm (.303 in) Vickers machine gun; 2 × trainable, rearward-firing 7.7 mm (.303 in) Lewis Guns for observer
Bombs weight (kg)
2
 
120
39,000
Stat
Number built (qt)
0
 
227
43,000
Introduction 1929
First flight 23.02.1929
Stop production 1939

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