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    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      45 kg/m2
      69 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
      2793 kg
      4191 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      147 km/h
      221 km/h
    • Max. Speed
      25 km/h
      28165 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
      920 hp
      1380 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2657 m
      3987 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1687 km
      2532 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
      12 min
      20 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
      3 qt
      5 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
      30 qt
    • Price
      41 USD
      750000000 USD

Douglas PD

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
15.0
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
22.2
95
Wing loading (kg/m2)
3.1
 
56.8
829
Weights
Empty weight (kg)
8
 
3,492.2
276,800
Capacity
Crew (per.)
1
 
5
112
Speeds
Ground Speed (km/h)
96.6
 
184
1,500
at sea level
Power
Total Power (hp)
0.4
 
1,150
60,000
2 powerplants 575 hp each
Performance
Service ceiling (m)
0.6
 
3,322.3
161,544
Range (Ferry range) (km)
4
 
2,109.4
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
16
105
to 1520 m
Combat
Guns (qt)
1
 
-1
18
Single .30 in (7.62 mm) calibre machine guns in bow and amidships cockpits
Bombs (qt)
1
 
4
250
105 kg bombs underwing
Stat
Number built (qt)
0
 
25
43,000
by Douglas
Introduction 1922

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