Search filter

    • Year
      1906
      2018
    • Length
      22 m
      35 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      108 m2
      164 m2
    • Wingspan (Beam)
      28 m
      43 m
    • Wing loading
      169 kg/m2
      255 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
      15712 kg
      23569 kg
    • Max. takeoff weight (Gross weight)
      26489 kg
      39735 kg
    • Loaded weight
      23040 kg
      34560 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      64 per.
      96 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      360 km/h
      540 km/h
    • Сruise Speed
      292 km/h
      438 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
      4640 hp
      6960 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5437 m
      8157 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5471 km
      8207 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      3218 km
      4828 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
      18 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
      64 qt
      96 qt
    • Price
      41 USD
      750000000 USD

Douglas DC-4

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
28.6
88.7
Height (m)
0.6
 
8.4
50.1
Wings
Wing area (m2)
1.1
 
135.9
925
Wingspan (Beam) (m)
0.1
 
35.8
95
Wing loading (kg/m2)
3.1
 
212.4
829
Weights
Empty weight (kg)
8
 
19,640.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
33,112.2
575,000
Loaded weight (kg)
5
 
28,800
242,500
Capacity
Crew (per.)
1
 
4
112
Capacity passengers (per.)
1
 
80
400
40 to 80 passengers
Speeds
Max. Speed (km/h)
25
 
450
28,165
Сruise Speed (km/h)
52
 
365
3,087
Power
Total Power (hp)
0.4
 
5,800
60,000
4 powerplants 1450 hp each
Performance
Service ceiling (m)
0.6
 
6,797.0
161,544
Range (Ferry range) (km)
4
 
6,839
40,700
Сombat radius (km)
277
 
4,023
7,210
Stat
Number built (qt)
0
 
80
43,000
Introduction 1942
First flight 14.02.1942

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