Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      36 m2
    • Wingspan (Beam)
      10 m
      16 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
      1671 kg
      2508 kg
    • Max. takeoff weight (Gross weight)
      2611 kg
      3918 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      285 km/h
      429 km/h
    • Сruise Speed
      247 km/h
      371 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
      660 hp
      990 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6169 m
      9254 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1481 km
      2223 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      708 km
      1062 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
      309 m/min
      465 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      363 kg
      545 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      44 qt
      66 qt
    • Price
      41 USD
      750000000 USD

Douglas DB-19

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.7
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
29.6
925
Wingspan (Beam) (m)
0.1
 
12.7
95
Weights
Empty weight (kg)
8
 
2,089.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,264.5
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and gunner
Speeds
Max. Speed (km/h)
25
 
357
28,165
at 2900 m
Сruise Speed (km/h)
52
 
309
3,087
Power
Total Power (hp)
0.4
 
825
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,711.4
161,544
Range (Ferry range) (km)
4
 
1,852
40,700
Сombat radius (km)
277
 
885
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
387.1
36,000
Combat
Guns (qt)
1
 
2
18
1 × .50 in (12.7 mm) machine gun; 1 × .30 in (7.62 mm) machine gun
Bombs weight (kg)
2
 
454
39,000
bomb under fuselage
Stat
Number built (qt)
0
 
55
43,000
Introduction 1935
First flight 19.08.1935

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