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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      70 m2
      105 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
      4274 kg
      6412 kg
    • Max. takeoff weight (Gross weight)
      6350 kg
      9526 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      9 per.
      15 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      270 km/h
      406 km/h
    • Сruise Speed
      244 km/h
      368 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
      1136 hp
      1704 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5608 m
      8413 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1288 km
      1932 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Douglas DC-1
TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
18.3
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
87.5
925
Wingspan (Beam) (m)
0.1
 
25.9
95
Weights
Empty weight (kg)
8
 
5,343.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,938
575,000
Capacity
Crew (per.)
1
 
2
112
pilots
Capacity passengers (per.)
1
 
12
400
Speeds
Max. Speed (km/h)
25
 
338
28,165
Сruise Speed (km/h)
52
 
306
3,087
at 2440 m
Power
Total Power (hp)
0.4
 
1,420
60,000
2 powerplants 710 hp each
Performance
Service ceiling (m)
0.6
 
7,010.4
161,544
Range (Ferry range) (km)
4
 
1,610
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1933
First flight 01.07.1933

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