Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      29 m2
      45 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      176 kg/m2
      264 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
      4342 kg
      6515 kg
    • Max. takeoff weight (Gross weight)
      9071 kg
      13608 kg
    • Loaded weight
      6570 kg
      9856 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      12 qt
      18 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      414 km/h
      622 km/h
    • Сruise Speed
      255 km/h
      383 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
      2160 hp
      3240 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6949 m
      10425 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1692 km
      2538 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
      696 m/min
      1044 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
      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
      2544 qt
      3816 qt
    • Price
      41 USD
      750000000 USD

Douglas A-1 Skyraider

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.8
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
37.2
925
Wingspan (Beam) (m)
0.1
 
15.3
95
Wing loading (kg/m2)
3.1
 
220
829
Weights
Empty weight (kg)
8
 
5,428.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,339.8
575,000
Loaded weight (kg)
5
 
8,213
242,500
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
15
2,576
external hardpoints
Speeds
Max. Speed (km/h)
25
 
518
28,165
at 5500 m
Сruise Speed (km/h)
52
 
319
3,087
Power
Total Power (hp)
0.4
 
2,681.0
60,000
0.4
 
2,700
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,686.8
161,544
Range (Ferry range) (km)
4
 
2,115
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
870
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) M2 cannon
Stat
Number built (qt)
0
 
3,180
43,000
Introduction 1949
First flight 18.03.1945
Stop production 1985

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