Search filter

    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      20 m
      32 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
      4519 kg
      6780 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      6736 kg
      10104 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      270 km/h
      406 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
      1168 hp
      1752 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5547 m
      8322 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1400 km
      2100 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
      251 m/min
      377 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
      158 qt
      238 qt
    • Price
      41 USD
      750000000 USD

Douglas DC-2

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
19.1
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wingspan (Beam) (m)
0.1
 
25.9
95
Weights
Empty weight (kg)
8
 
5,649.5
276,800
Loaded weight (kg)
5
 
8,420
242,500
Capacity
Capacity passengers (per.)
1
 
14
400
Speeds
Max. Speed (km/h)
25
 
338
28,165
at 2073 m
Power
Total Power (hp)
0.4
 
1,460
60,000
2 powerplants 730 hp each
Performance
Service ceiling (m)
0.6
 
6,934.2
161,544
Range (Ferry range) (km)
4
 
1,750
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
313.9
36,000
Stat
Number built (qt)
0
 
198
43,000
First flight 11.05.1934

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