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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      38 m2
    • Wingspan (Beam)
      12 m
      19 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
      2445 kg
      3669 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3834 kg
      5752 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      544 kg
      816 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      240 km/h
      360 km/h
    • Сruise Speed
      220 km/h
      330 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
      704 hp
      1056 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5117 m
      7677 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1200 km
      1800 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
      278 m/min
      418 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
      2 qt
      4 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
      96 qt
      146 qt
    • Price
      41 USD
      750000000 USD

Latécoère 298

TypeAircraft
Company

Groupe Latécoère

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.6
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
31.6
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Weights
Empty weight (kg)
8
 
3,057
276,800
Loaded weight (kg)
5
 
4,793
242,500
Capacity
Crew (per.)
1
 
3
112
2 to 4, usually 3
Payload (kg)
23
 
680
122,470
Speeds
Max. Speed (km/h)
25
 
300
28,165
Сruise Speed (km/h)
52
 
275
3,087
Power
Total Power (hp)
0.4
 
880
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,397
161,544
Range (Ferry range) (km)
4
 
1,500
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
348
36,000
Combat
Guns (qt)
1
 
3
18
7.5 mm Darne machine guns
Stat
Number built (qt)
0
 
121
43,000
Introduction 1939
First flight 06.05.1936
Stop production 1951

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