Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      24 m2
      36 m2
    • Wingspan (Beam)
      9 m
      15 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
      832 kg
      1248 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1228 kg
      1842 kg
    • Crew
      1 per.
      2 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
      25 km/h
      28165 km/h
    • Сruise Speed
      52 km/h
      3087 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
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      3 qt
    • Guns
      3 qt
      5 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
      2 qt
    • Price
      41 USD
      750000000 USD

Dewoitine D.15

Company

Société Aéronautique Française (Avions Dewoitine)

Geometry
Length (m)
1.9
 
7.4
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
30
925
Wingspan (Beam) (m)
0.1
 
12
95
Weights
Empty weight (kg)
8
 
1,040
276,800
Loaded weight (kg)
5
 
1,535
242,500
Capacity
Crew (per.)
1
 
1
112
Power
Total Power (hp)
0.4
 
450
60,000
1 powerplant
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
2
8
Combat
Guns (qt)
1
 
4
18
2 × 7.7 mm (0.303 in) synchronised Vickers machine gun on fuselage, firing through propeller arc and 2 × 7.5 mm (0.295 in) Darne machine guns on upper wing centre section
Stat
Number built (qt)
0
 
1
43,000
First flight 13.08.1924

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