Search filter

    • Year
      1906
      2018
    • Length
      31 m
      48 m
    • Height
      11 m
      18 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      186 m2
      280 m2
    • Wingspan (Beam)
      42 m
      64 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
      36710 kg
      55066 kg
    • Max. takeoff weight (Gross weight)
      70578 kg
      105869 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 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
      391 km/h
      587 km/h
    • Сruise Speed
      296 km/h
      444 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
      12160 hp
      18240 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5315 m
      7974 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      8780 km
      13170 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
      185 m/min
      278 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
      18 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
      358 qt
      538 qt
    • Price
      41 USD
      750000000 USD

Douglas C-124 Globemaster II

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
39.8
88.7
Height (m)
0.6
 
14.7
50.1
Wings
Wing area (m2)
1.1
 
233.1
925
Wingspan (Beam) (m)
0.1
 
53.1
95
Weights
Empty weight (kg)
8
 
45,887.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
88,223.7
575,000
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
489
28,165
at 6340
Сruise Speed (km/h)
52
 
370
3,087
Power
Total Power (hp)
0.4
 
15,200
60,000
4 powerplants 3800 hp each
Performance
Service ceiling (m)
0.6
 
6,644.6
161,544
Range (Ferry range) (km)
4
 
10,975
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
231.7
36,000
Stat
Number built (qt)
0
 
448
43,000
Introduction 1949
First flight 27.11.1949
Stop production 1974

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