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    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      91 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      336 kg/m2
      506 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
      14300 kg
      21451 kg
    • Max. takeoff weight (Gross weight)
      29755 kg
      44634 kg
    • Loaded weight
      25400 kg
      38100 kg
    • Crew
      2 per.
      4 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
      785 km/h
      1179 km/h
    • Сruise Speed
      669 km/h
      1005 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
      88 kN/kg
      133 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      37 kN
      57 kN
    • Service ceiling
      9996 m
      14994 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2704 km
      4056 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
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      4640 kg
      6960 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      225 qt
      339 qt
    • Price
      41 USD
      750000000 USD

Douglas A-3 Skywarrior

TypeAircraft
Company

Douglas Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
23.3
88.7
Height (m)
0.6
 
7.0
50.1
Wings
Wing area (m2)
1.1
 
75.4
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Wing loading (kg/m2)
3.1
 
421
829
Weights
Empty weight (kg)
8
 
17,875.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,194.6
575,000
Loaded weight (kg)
5
 
31,750
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
982
28,165
at 3050 m
Сruise Speed (km/h)
52
 
837
3,087
Power
Afterburning thrust (kN/kg)
29.4
 
110.6
980
2 powerplants 55,3 kN each
Thrust (kN)
1.5
 
46.7
1,914
2 powerplants 46,7 kN each
Performance
Service ceiling (m)
0.6
 
12,495
161,544
Range (Ferry range) (km)
4
 
3,380
40,700
Combat
Guns (qt)
1
 
2
18
20 mm M3L cannon in the tail turret
Bombs weight (kg)
2
 
5,800
39,000
of free-fall bombs or mines
Stat
Number built (qt)
0
 
282
43,000
Introduction 1952
First flight 28.10.1952
Stop production 27.09.1991

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