Search filter

    • Year
      1906
      2018
    • Length
      3 m
      5 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      38 m2
      59 m2
    • Wingspan (Beam)
      13 m
      21 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
      1272 kg
      1908 kg
    • Max. takeoff weight (Gross weight)
      2691 kg
      4037 kg
    • Loaded weight
      2691 kg
      4037 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      150 km/h
      226 km/h
    • Сruise Speed
      125 km/h
      189 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
      360 hp
      540 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3800 m
      5700 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      544 km
      816 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
      72 qt
      108 qt
    • Price
      41 USD
      750000000 USD

Latécoère 26

TypeAircraft
Company

Groupe Latécoère

Scheme

Parasol

Monoplane

Geometry
Length (m)
1.9
 
3.9
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
48.6
925
Wingspan (Beam) (m)
0.1
 
17.4
95
Weights
Empty weight (kg)
8
 
1,590
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,364
575,000
Loaded weight (kg)
5
 
3,364
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Speeds
Max. Speed (km/h)
25
 
188
28,165
Сruise Speed (km/h)
52
 
157
3,087
Power
Total Power (hp)
0.4
 
450
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,750
161,544
Range (Ferry range) (km)
4
 
680
40,700
Stat
Number built (qt)
0
 
90
43,000
Introduction 1927
First flight 1926

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