Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      18 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      22 kg/m2
      34 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      16
      24
    • 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
      212 kg
      318 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      344 kg
      516 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
      176 km/h
      264 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      49 km/h
      75 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      176 km/h
      264 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
      28
      42
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      44 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
      28 qt
      44 qt
    • Price
      41 USD
      750000000 USD

Breguet 901 Mouette

TypeGlider
Company

Breguet Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
7.6
88.7
Wings
Wing area (m2)
1.1
 
15
925
Wingspan (Beam) (m)
0.1
 
17.3
95
Wing loading (kg/m2)
3.1
 
28
829
Aspect ratio
1.7
 
20
25.6
Weights
Empty weight (kg)
8
 
265
276,800
Loaded weight (kg)
5
 
430
242,500
Capacity
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
220
28,165
Stall Speed (km/h)
40
 
62
257.7
Never exceed speed (km/h)
108.0
 
220
1,050
Performance
Maximum glide ratio
7
 
35
43
at 85 km/h
Dynamic Performance
Rate of sink (m/min)
36
 
36
55.8
at 72 km/h
Stat
Number built (qt)
0
 
36
43,000
Introduction 1954
First flight 11.03.1954

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