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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      104 m2
      156 m2
    • Wingspan (Beam)
      25 m
      38 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
      4380 kg
      6570 kg
    • Max. takeoff weight (Gross weight)
      7770 kg
      11656 kg
    • Loaded weight
      7580 kg
      11370 kg
    • Crew
      2 per.
      4 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
      167 km/h
      251 km/h
    • Сruise Speed
      115 km/h
      173 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
      1096 hp
      1644 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3760 m
      5640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1440 km
      2160 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
      4 qt
      6 qt
    • Price
      41 USD
      750000000 USD

Latécoère 380

TypeFlying boat
Company

Groupe Latécoère

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
17.2
88.7
Height (m)
0.6
 
5.5
50.1
Wings
Wing area (m2)
1.1
 
130
925
Wingspan (Beam) (m)
0.1
 
31.4
95
Weights
Empty weight (kg)
8
 
5,475
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,713
575,000
Loaded weight (kg)
5
 
9,475
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
209
28,165
Сruise Speed (km/h)
52
 
144
3,087
Power
Total Power (hp)
0.4
 
1,370
60,000
2 powerplants 685 hp each
Performance
Service ceiling (m)
0.6
 
4,700
161,544
Range (Ferry range) (km)
4
 
1,800
40,700
Stat
Number built (qt)
0
 
5
43,000
Introduction 1930
First flight 24.08.1930

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