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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      73 m2
      111 m2
    • Wingspan (Beam)
      22 m
      34 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
      6926 kg
      10391 kg
    • Max. takeoff weight (Gross weight)
      11757 kg
      17636 kg
    • Loaded weight
      9616 kg
      14425 kg
    • Crew
      4 per.
      8 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
      96 km/h
      1500 km/h
    • Max. Speed
      363 km/h
      545 km/h
    • Сruise Speed
      270 km/h
      406 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
      2560 hp
      3840 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7704 m
      11556 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1802 km
      2704 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
      5 min
      9 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      728 kg
      1092 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      30 qt
      46 qt
    • Price
      41 USD
      750000000 USD

Douglas B-23 Dragon

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
17.8
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
92.3
925
Wingspan (Beam) (m)
0.1
 
28.0
95
Weights
Empty weight (kg)
8
 
8,658.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,696.4
575,000
Loaded weight (kg)
5
 
12,020.2
242,500
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
453.8
28,165
at 3660 m
Сruise Speed (km/h)
52
 
338.0
3,087
Power
Total Power (hp)
0.4
 
3,200
60,000
2 powerplants 1600 hp each
Performance
Service ceiling (m)
0.6
 
9,630
161,544
Range (Ferry range) (km)
4
 
2,253
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
6.7
105
to 3050 m
Combat
Guns (qt)
1
 
4
18
3 × .30 in (7.62 mm) machine guns; 1 × .50 in (12.7 mm) machine gun in tail
Bombs weight (kg)
2
 
910
39,000
in bomb bay
Stat
Number built (qt)
0
 
38
43,000
Introduction 1939
First flight 27.07.1939

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