Search filter

    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      23 m
      36 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
      6580 kg
      9872 kg
    • Max. takeoff weight (Gross weight)
      11249 kg
      16874 kg
    • Loaded weight
      9434 kg
      14152 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      2177 kg
      3266 kg
    • Payload
      2177 kg
      3266 kg
    • Capacity passengers
      22 per.
      34 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      288 km/h
      432 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
      7 hp
      12 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6437 m
      9657 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2060 km
      3090 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
      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
      8000 qt
      12000 qt
    • Price
      41 USD
      750000000 USD

Douglas C-47 Skytrain

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
19.4
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wingspan (Beam) (m)
0.1
 
29.4
95
Weights
Empty weight (kg)
8
 
8,225.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,061.4
575,000
Loaded weight (kg)
5
 
11,793
242,500
Capacity
Useful load (kg)
26.4
 
2,721.6
90,700
Payload (kg)
23
 
2,721.6
122,470
Capacity passengers (per.)
1
 
28
400
troops
Speeds
Max. Speed (km/h)
25
 
360
28,165
at 3050 m
Power
Total Power (hp)
0.4
 
2,400
60,000
2 powerplants 1200 hp each
0.4
 
9.5
60,000
to 3050 m
Performance
Service ceiling (m)
0.6
 
8,046.7
161,544
Range (Ferry range) (km)
4
 
2,575
40,700
Stat
Number built (qt)
0
 
10,000
43,000
First flight 23.12.1941

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