Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      44 m2
    • Wingspan (Beam)
      11 m
      18 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
      1208 kg
      1812 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1712 kg
      2568 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      131 km/h
      197 km/h
    • Сruise Speed
      105 km/h
      159 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
      224 hp
      336 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3440 m
      5160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      480 km
      720 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
      19 qt
      29 qt
    • Price
      41 USD
      750000000 USD

Latécoère 17

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
9.6
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
36
925
Wingspan (Beam) (m)
0.1
 
14.7
95
Weights
Empty weight (kg)
8
 
1,510
276,800
Loaded weight (kg)
5
 
2,140
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
164
28,165
Сruise Speed (km/h)
52
 
132
3,087
Power
Total Power (hp)
0.4
 
280
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,300
161,544
Range (Ferry range) (km)
4
 
600
40,700
Stat
Number built (qt)
0
 
24
43,000
Introduction 1924
First flight 01.10.1923

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