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    • Year
      1906
      2018
    • Length
      21 m
      33 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      156 m2
      235 m2
    • Wingspan (Beam)
      32 m
      49 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
      12827 kg
      19241 kg
    • Max. takeoff weight (Gross weight)
      24852 kg
      37278 kg
    • Loaded weight
      21244 kg
      31866 kg
    • Crew
      5 per.
      9 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
      279 km/h
      419 km/h
    • Сruise Speed
      144 km/h
      216 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
      3155 hp
      4733 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3400 km
      5100 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      25 h
      39 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
      8 min
      12 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      5 qt
      9 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      641 kg
      963 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Latécoère 611

TypeFlying boat
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
27.1
88.7
Height (m)
0.6
 
7.7
50.1
Wings
Wing area (m2)
1.1
 
195.1
925
Wingspan (Beam) (m)
0.1
 
40.6
95
Weights
Empty weight (kg)
8
 
16,034
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
31,065
575,000
Loaded weight (kg)
5
 
26,555
242,500
Capacity
Crew (per.)
1
 
7
112
Speeds
Max. Speed (km/h)
25
 
349
28,165
Сruise Speed (km/h)
52
 
180
3,087
Power
Total Power (hp)
0.4
 
3,944
60,000
4 powerplants 986 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Range (Ferry range) (km)
4
 
4,250
40,700
Endurance (h)
0.0
 
32
150
Dynamic Performance
Time to altitude (min)
0.6
 
10
105
to 2000 m
Combat
Guns (qt)
1
 
7
18
2 x 12.7 mm (0.50 in) Machine guns in dorsal turret; 1 x 12.7 mm (0.50 in) Browning M2 mchine gun in a tail position; 4 x 7.5 mm (0.30 in) Darne machine guns in beam positions
Bombs weight (kg)
2
 
802
39,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1939
First flight 08.03.1939
Stop production 1947

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