Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      59 m2
      90 m2
    • Wingspan (Beam)
      44 m
      68 m
    • Wing loading
      31 kg/m2
      47 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
      1416 kg
      2124 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2337 kg
      3507 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      880 kg
      1320 kg
    • Capacity passengers
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      149 km/h
      225 km/h
    • Сruise Speed
      109 km/h
      165 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
      348 hp
      522 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3621 m
      5432 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      496 km
      745 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
      157 m/min
      236 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
      20 qt
      32 qt
    • Price
      41 USD
      750000000 USD

Douglas C-1

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.8
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
74.8
925
Wingspan (Beam) (m)
0.1
 
56
95
Wing loading (kg/m2)
3.1
 
39.1
829
Weights
Empty weight (kg)
8
 
1,770
276,800
Loaded weight (kg)
5
 
2,922
242,500
Capacity
Crew (per.)
1
 
2
112
Payload (kg)
23
 
1,100
122,470
Capacity passengers (per.)
1
 
6
400
or cargo
Speeds
Max. Speed (km/h)
25
 
187
28,165
Сruise Speed (km/h)
52
 
137
3,087
Power
Total Power (hp)
0.4
 
435
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,526.3
161,544
Range (Ferry range) (km)
4
 
620.4
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
196.6
36,000
Stat
Number built (qt)
0
 
26
43,000
Introduction 1925
First flight 02.05.1925

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