Search filter

    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      16 m2
    • Wingspan (Beam)
      11 m
      18 m
    • Wing loading
      19 kg/m2
      29 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      12
      20
    • 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
      168 kg
      254 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      244 kg
      368 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      144 km/h
      216 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      48 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
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 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
      21
      33
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      54 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      6 qt
      10 qt
    • Price
      41 USD
      750000000 USD

Breguet 900 Louisette

Company

Breguet Aviation

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
6.5
88.7
Wings
Wing area (m2)
1.1
 
12.9
925
Wingspan (Beam) (m)
0.1
 
14.4
95
Wing loading (kg/m2)
3.1
 
23.8
829
Aspect ratio
1.7
 
15.9
25.6
Weights
Empty weight (kg)
8
 
211
276,800
Loaded weight (kg)
5
 
306
242,500
Capacity
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
180
28,165
Stall Speed (km/h)
40
 
40
257.7
with 30° flaps
Performance
Maximum glide ratio
7
 
27
43
at 78 km/h
Dynamic Performance
Rate of sink (m/min)
36
 
45
55.8
at 78 km/h
Stat
Number built (qt)
0
 
8
43,000
First flight 17.06.1948

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