Search filter

    • Year
      1906
      2018
    • Length
      20 m
      32 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      208 m2
      312 m2
    • Wingspan (Beam)
      35 m
      53 m
    • Wing loading
      74 kg/m2
      112 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
      11472 kg
      17208 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      19240 kg
      28860 kg
    • Crew
      6 per.
      10 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
      192 km/h
      288 km/h
    • Сruise Speed
      148 km/h
      222 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
      2976 hp
      4464 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4000 m
      6000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2640 km
      3960 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      16 h
      24 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
      6 qt
      9 qt
    • Bombs
      3 qt
      5 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
      5 qt
      9 qt
    • Price
      41 USD
      750000000 USD

Latécoère 300

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

Parasol

Geometry
Length (m)
1.9
 
26.2
88.7
Height (m)
0.6
 
8.0
50.1
Wings
Wing area (m2)
1.1
 
260
925
Wingspan (Beam) (m)
0.1
 
44.0
95
Wing loading (kg/m2)
3.1
 
93.2
829
Weights
Empty weight (kg)
8
 
14,340
276,800
Loaded weight (kg)
5
 
24,050
242,500
Capacity
Crew (per.)
1
 
8
112
Speeds
Max. Speed (km/h)
25
 
240
28,165
at 2000 m
Сruise Speed (km/h)
52
 
185
3,087
Power
Total Power (hp)
0.4
 
3,720
60,000
4 powerplants 930 hp each
Performance
Service ceiling (m)
0.6
 
5,000
161,544
Range (Ferry range) (km)
4
 
3,300
40,700
Endurance (h)
0.0
 
20
150
at 150 km/h
Combat
Guns (qt)
1
 
7.5
18
7.5 mm (0.3 in) Darne machine gun in bow, 2 firing through beam windows
Bombs (qt)
1
 
4
250
75 kg (165 lb) bombs
Stat
Number built (qt)
0
 
7
43,000
Introduction 1932
First flight 1931

Similar aircraft

Get more

Comments