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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      41 m2
    • Wingspan (Beam)
      11 m
      18 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
      1768 kg
      2653 kg
    • Max. takeoff weight (Gross weight)
      2736 kg
      4106 kg
    • Loaded weight
      2662 kg
      3994 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
      265 km/h
      399 km/h
    • Сruise Speed
      219 km/h
      329 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
      600 hp
      900 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4730 m
      7096 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      836 km
      1256 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
      329 m/min
      494 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
      4 qt
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      435 kg
      653 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      328 qt
      494 qt
    • Price
      41 USD
      750000000 USD

Douglas Model_8

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.7
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
33.6
925
Wingspan (Beam) (m)
0.1
 
14.5
95
Weights
Empty weight (kg)
8
 
2,210.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,421
575,000
Loaded weight (kg)
5
 
3,328
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and gunner
Speeds
Max. Speed (km/h)
25
 
332
28,165
Сruise Speed (km/h)
52
 
274
3,087
Power
Total Power (hp)
0.4
 
750
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,913.1
161,544
Range (Ferry range) (km)
4
 
1,046
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
411.5
36,000
Combat
Guns (qt)
1
 
5
18
4 × 0.3 in (7.62 mm) fixed forward M1919 Browning machine guns; 1 × 0.3 in (7.62 mm) trainable rear machine gun
Bombs weight (kg)
2
 
544
39,000
Stat
Number built (qt)
0
 
411
43,000
Introduction 1934

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