Search filter

    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      103 m2
      155 m2
    • Wingspan (Beam)
      27 m
      41 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
      5811 kg
      8717 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      8455 kg
      12683 kg
    • Crew
      4 per.
      6 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
      201 km/h
      303 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      152 km/h
      228 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
      1600 hp
      2400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      800 km
      1200 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
      196 m/min
      296 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1200 kg
      1800 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Latécoère 550

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
19.8
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
129
925
Wingspan (Beam) (m)
0.1
 
34.0
95
Weights
Empty weight (kg)
8
 
7,264
276,800
up to 7,305 kg depending on equipment
Loaded weight (kg)
5
 
10,569
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Ground Speed (km/h)
96.6
 
252
1,500
at 100 m
Сruise Speed (km/h)
52
 
190
3,087
Power
Total Power (hp)
0.4
 
2,000
60,000
4 powerplants 500 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Сombat radius (km)
277
 
1,000
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
246
36,000
to 4000 m
Combat
Guns (qt)
1
 
1
18
7.7 mm (0.303 in) Lewis machine gun in each of the turrets and in the open ventral position.
Bombs weight (kg)
2
 
1,500
39,000
Bombs and torpedoes
Stat
Number built (qt)
0
 
1
43,000
Introduction 1933
First flight 29.04.1933

Similar aircraft

Get more

Comments