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    • 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
      73 m2
      111 m2
    • Wingspan (Beam)
      23 m
      35 m
    • Wing loading
      100 kg/m2
      150 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
      3 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
      6119 kg
      9180 kg
    • Max. takeoff weight (Gross weight)
      11260 kg
      16890 kg
    • Loaded weight
      9144 kg
      13716 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      25 per.
      39 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      296 km/h
      445 km/h
    • Сruise Speed
      266 km/h
      400 km/h
    • Stall Speed
      86 km/h
      130 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
      2988 l
      4484 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1760 hp
      2640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5680 m
      8520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2029 km
      3045 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
      273 m/min
      411 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
      2 m
      5 m
    • Prop blade number
      2 qt
      4 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
      485 qt
      729 qt
    • Price
      63600 USD
      95400 USD

Douglas DC-3

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
19.7
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wing area (m2)
1.1
 
91.7
925
Wingspan (Beam) (m)
0.1
 
29
95
Wing loading (kg/m2)
3.1
 
125
829
Rotors
Rotor number (qt)
1
 
2
8
Weights
Empty weight (kg)
8
 
7,649.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,075
575,000
Loaded weight (kg)
5
 
11,430
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
32
400
21–32 passengers
Speeds
Max. Speed (km/h)
25
 
370.2
28,165
at 2590
Сruise Speed (km/h)
52
 
333.1
3,087
Stall Speed (km/h)
40
 
108
257.7
Fuel
Fuel Capacity (l)
23
 
3,736
320,000
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
2,200
60,000
2 powerplants 1100 hp each
Performance
Service ceiling (m)
0.6
 
7,100
161,544
Range (Ferry range) (km)
4
 
2,537.2
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
342
36,000
Propellers
Prop diameter (m)
1.8
 
3.5
5.8
Prop blade number (qt)
1
 
3
8
Stat
Number built (qt)
0
 
607
43,000
Price (USD)
41.5
 
79,500
750.0 million
Introduction 1951
First flight 17.12.1935

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