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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      73 m2
      111 m2
    • Wingspan (Beam)
      23 m
      35 m
    • Wing loading
      130 kg/m2
      195 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
      6560 kg
      9842 kg
    • Max. takeoff weight (Gross weight)
      11976 kg
      17964 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      6 per.
      10 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
      300 km/h
      450 km/h
    • Сruise Speed
      224 km/h
      336 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
      1920 hp
      2880 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5961 m
      8943 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2800 km
      4201 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1948 km
      2922 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
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      8 qt
      12 qt
    • Bombs
      1 qt
      250 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
      42 qt
      64 qt
    • Price
      41 USD
      750000000 USD

Douglas AC-47 Spooky

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
19.6
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wing area (m2)
1.1
 
91.7
925
Wingspan (Beam) (m)
0.1
 
28.9
95
Wing loading (kg/m2)
3.1
 
162.5
829
Weights
Empty weight (kg)
8
 
8,201.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,970
575,000
Capacity
Crew (per.)
1
 
8
112
pilot, copilot, navigator, flight engineer, loadmaster, 2 gunners and a South Vietnamese observer (during Vietnam war)
Speeds
Max. Speed (km/h)
25
 
375
28,165
Сruise Speed (km/h)
52
 
280
3,087
Power
Total Power (hp)
0.4
 
2,400
60,000
2 powerplants 1200 each
Performance
Service ceiling (m)
0.6
 
7,452.4
161,544
Range (Ferry range) (km)
4
 
3,500.3
40,700
Сombat radius (km)
277
 
2,435
7,210
Combat
Guns (qt)
1
 
3
18
7.62 mm General Electric GAU-2/M134 miniguns or
1
 
10
18
.30 in Browning AN/M2 machine guns
Stat
Number built (qt)
0
 
53
43,000
Introduction 1964

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