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    • Year
      1906
      2018
    • Length
      38 m
      58 m
    • Height
      11 m
      18 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      198 m2
      299 m2
    • Wingspan (Beam)
      43 m
      66 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
      39704 kg
      59557 kg
    • Max. takeoff weight (Gross weight)
      103781 kg
      155673 kg
    • Loaded weight
      100000 kg
      150000 kg
    • Crew
      4 per.
      8 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      40000 kg
      60000 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      462 km/h
      694 km/h
    • Сruise Speed
      415 km/h
      623 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
      24000 hp
      36000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7876 m
      11815 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5274 km
      7912 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
      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
      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
      40 qt
      60 qt
    • Price
      41 USD
      750000000 USD

Douglas C-133 Cargomaster

TypeAircraft
Company

Douglas Aircraft Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
48
88.7
Height (m)
0.6
 
14.7
50.1
Wings
Wing area (m2)
1.1
 
248.3
925
Wingspan (Beam) (m)
0.1
 
54.8
95
Weights
Empty weight (kg)
8
 
49,630.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
129,727.4
575,000
Loaded weight (kg)
5
 
125,000
242,500
Capacity
Crew (per.)
1
 
6
112
two pilots, navigator, two flight engineers, loadmaster
Payload (kg)
23
 
50,000
122,470
Speeds
Max. Speed (km/h)
25
 
578
28,165
Сruise Speed (km/h)
52
 
519
3,087
Power
Total Power (hp)
0.4
 
30,000
60,000
4 powerplants 7500 hp each
Performance
Service ceiling (m)
0.6
 
9,845.0
161,544
Range (Ferry range) (km)
4
 
6,593.1
40,700
with 23587 kg payload
Stat
Number built (qt)
0
 
50
43,000
Introduction 1956
First flight 23.04.1956
Stop production 1971

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