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    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      38 m2
      59 m2
    • Wingspan (Beam)
      15 m
      24 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
      1732 kg
      2600 kg
    • Max. takeoff weight (Gross weight)
      3232 kg
      4848 kg
    • Loaded weight
      3084 kg
      4628 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      740 kg
      1110 kg
    • Payload
      740 kg
      1110 kg
    • Capacity passengers
      6 per.
      10 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      177 km/h
      267 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      160 km/h
      240 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4160 m
      6240 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3748 km
      5622 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
      97 m/min
      147 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      47 min
      72 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Latécoère 28

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
13.6
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
48.6
925
Wingspan (Beam) (m)
0.1
 
19.3
95
Weights
Empty weight (kg)
8
 
2,166
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,040
575,000
Loaded weight (kg)
5
 
3,856
242,500
Capacity
Crew (per.)
1
 
2
112
Useful load (kg)
26.4
 
925
90,700
Payload (kg)
23
 
925
122,470
Capacity passengers (per.)
1
 
8
400
Speeds
Ground Speed (km/h)
96.6
 
222
1,500
Сruise Speed (km/h)
52
 
200
3,087
Power
Total Power (hp)
0.4
 
500
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,200
161,544
Range (Ferry range) (km)
4
 
4,685
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
122.4
36,000
Time to altitude (min)
0.6
 
59.6
105
to 4000 m
Stat
Introduction 1929
First flight 1927

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