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    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      46 m2
      71 m2
    • Wingspan (Beam)
      15 m
      24 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
      2465 kg
      3699 kg
    • Max. takeoff weight (Gross weight)
      4144 kg
      6218 kg
    • Loaded weight
      4144 kg
      6218 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
      180 km/h
      270 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      136 km/h
      204 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
      520 hp
      780 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      632 km
      948 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
      97 m/min
      147 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      3 m
      6 m
    • Prop blade number
      1 qt
      3 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Latécoère 440

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Parasol

Geometry
Length (m)
1.9
 
14.1
88.7
Height (m)
0.6
 
5.5
50.1
Wings
Wing area (m2)
1.1
 
58.4
925
Wingspan (Beam) (m)
0.1
 
19.3
95
Weights
Empty weight (kg)
8
 
3,082
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,181
575,000
Loaded weight (kg)
5
 
5,181
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
225
1,500
Сruise Speed (km/h)
52
 
170
3,087
at sea level
Power
Total Power (hp)
0.4
 
650
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Сombat radius (km)
277
 
790
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
122.4
36,000
to 2000 m
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
4.2
5.8
Prop blade number (qt)
1
 
2
8
Combat
Guns (qt)
1
 
6
18
2×forward firing 7.7 mm (0.303 in) Vickers machine guns, replenishable from bomb aimer's position; 2×movable 7.7 mm (0.303 in) Lewis guns in dorsal cupola; 2×movable 7.7 mm (0.303 in) Lewis guns in ventral position
Bombs (qt)
1
 
2
250
420 kg bombs or
Torpedoes (qt)
1
 
1
4
700 kg torpedo under centre section, off-set to starboard
Stat
Number built (qt)
0
 
2
43,000
Introduction 1931
First flight 1931

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