Search filter

    • Year
      1906
      2018
    • Length
      17 m
      26 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      21 m
      33 m
    • Wing loading
      71 kg/m2
      107 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
      5094 kg
      7642 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      7200 kg
      10800 kg
    • Crew
      1 per.
      112 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
      217 km/h
      327 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      96 km/h
      144 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
      1280 hp
      1920 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4608 m
      6913 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
      187 m/min
      282 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Douglas YOA-5

TypeAircraft
Company

Douglas Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
21.3
88.7
Height (m)
0.6
 
6.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
27.4
95
Wing loading (kg/m2)
3.1
 
89
829
Weights
Empty weight (kg)
8
 
6,367.5
276,800
Loaded weight (kg)
5
 
9,000
242,500
Speeds
Max. Speed (km/h)
25
 
272
28,165
Stall Speed (km/h)
40
 
120
257.7
Power
Total Power (hp)
0.4
 
1,600
60,000
2 powerplants 800 hp each
Performance
Service ceiling (m)
0.6
 
5,760.7
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
234.7
36,000
Combat
Guns (qt)
1
 
3
18
.30 in (7.62 mm) machine guns
Stat
Number built (qt)
0
 
1
43,000
First flight 1935
Stop production 1943

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