Search filter

    • 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
      34 m2
      52 m2
    • Wingspan (Beam)
      14 m
      23 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
      5461 kg
      8193 kg
    • Max. takeoff weight (Gross weight)
      9872 kg
      14808 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      436 km/h
      656 km/h
    • Сruise Speed
      281 km/h
      423 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
      5779 m
      8669 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1352 km
      2028 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
      487 m/min
      732 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
      7 qt
      11 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
      5982 qt
      8974 qt
    • Price
      41 USD
      750000000 USD

Douglas A-20 Havoc

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
14.6
88.7
Height (m)
0.6
 
5.4
50.1
Wings
Wing area (m2)
1.1
 
43.2
925
Wingspan (Beam) (m)
0.1
 
18.7
95
Weights
Empty weight (kg)
8
 
6,827.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,340
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
546
28,165
at 3050 m
Сruise Speed (km/h)
52
 
352
3,087
Power
Total Power (hp)
0.4
 
3,200
60,000
2 powerplants 1600 each
Performance
Service ceiling (m)
0.6
 
7,223.8
161,544
Range (Ferry range) (km)
4
 
1,690
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
609.6
36,000
Combat
Guns (qt)
1
 
9
18
6× fixed forward firing (12.7 mm).5in Browning machine guns in the nose; 2× flexible 0.5 in (12.7 mm) Browning machine guns, mounted dorsally; 1x flexible 0.5 in (12.7 mm) Browning machine gun, mounted behind bomb bay
Bombs weight (kg)
2
 
910
39,000
Stat
Number built (qt)
0
 
7,478
43,000
Introduction 1940
First flight 23.01.1939
Stop production 1949

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