Search filter

    • Year
      1906
      2018
    • Length
      34 m
      53 m
    • Height
      8 m
      13 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      280 m2
      420 m2
    • Wingspan (Beam)
      45 m
      69 m
    • Wing loading
      74 kg/m2
      112 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
      25920 kg
      38880 kg
    • Max. takeoff weight (Gross weight)
      57616 kg
      86424 kg
    • Loaded weight
      57080 kg
      85620 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      36 per.
      56 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      315 km/h
      473 km/h
    • Сruise Speed
      237 km/h
      357 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
      7680 hp
      11520 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5760 m
      8640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4828 km
      7242 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
      1 m/min
      36000 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
      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
      8 qt
      14 qt
    • Price
      41 USD
      750000000 USD

Latécoère 631

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
43.5
88.7
Height (m)
0.6
 
10.1
50.1
Wings
Wing area (m2)
1.1
 
350
925
Wingspan (Beam) (m)
0.1
 
57.4
95
Wing loading (kg/m2)
3.1
 
92.7
829
Weights
Empty weight (kg)
8
 
32,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
72,020
575,000
Loaded weight (kg)
5
 
71,350
242,500
Capacity
Crew (per.)
1
 
5
112
Capacity passengers (per.)
1
 
46
400
Speeds
Max. Speed (km/h)
25
 
394
28,165
Сruise Speed (km/h)
52
 
297
3,087
Power
Total Power (hp)
0.4
 
9,600
60,000
6 powerplants 1600 hp each
Performance
Service ceiling (m)
0.6
 
7,200
161,544
Range (Ferry range) (km)
4
 
6,035
40,700
Stat
Number built (qt)
0
 
11
43,000
10 + 1 prototype
Introduction 1942
First flight 04.11.1942

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