Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      59 m2
      90 m2
    • Wingspan (Beam)
      17 m
      27 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
      3520 kg
      5280 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5200 kg
      7800 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      190 km/h
      287 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      160 km/h
      240 km/h
    • Stall Speed
      91 km/h
      137 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
      960 hp
      1440 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5000 m
      7500 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Latécoère 350

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
15.0
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
74.8
925
Wingspan (Beam) (m)
0.1
 
22.4
95
Weights
Empty weight (kg)
8
 
4,400
276,800
Loaded weight (kg)
5
 
6,500
242,500
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
10
400
Speeds
Ground Speed (km/h)
96.6
 
238.5
1,500
Сruise Speed (km/h)
52
 
200
3,087
Stall Speed (km/h)
40
 
114
257.7
Power
Total Power (hp)
0.4
 
1,200
60,000
3 powerplants 400 hp each
Performance
Service ceiling (m)
0.6
 
6,250
161,544
Range (Ferry range) (km)
4
 
800
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1931
First flight 02.02.1931

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