Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      8 m
      13 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
      1161 kg
      1742 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1845 kg
      2768 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      3 per.
      5 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      294 km/h
      443 km/h
    • Сruise Speed
      257 km/h
      387 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5413 m
      8121 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1223 km
      1835 km
    • Range PTB (Ferry range)
      1512 km
      2270 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
      364 m/min
      548 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 Cloudster II

Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Concept

Geometry
Length (m)
1.9
 
12.1
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
10.8
95
Weights
Empty weight (kg)
8
 
1,451.5
276,800
Loaded weight (kg)
5
 
2,306.5
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
4
400
Speeds
Max. Speed (km/h)
25
 
368.5
28,165
at 365 m
Сruise Speed (km/h)
52
 
321.9
3,087
Power
Total Power (hp)
0.4
 
500
60,000
2 powerplants 250 hp each
Performance
Service ceiling (m)
0.6
 
6,767
161,544
Range (Ferry range) (km)
4
 
1,529
40,700
Range PTB (Ferry range) (km)
720
 
1,891.0
10,000
Dynamic Performance
Rate of climb (m/min)
1.9
 
456
36,000
Stat
Number built (qt)
0
 
1
43,000
First flight 12.03.1947

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