Search filter

    • Year
      1906
      2018
    • Length
      27 m
      42 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      117 m2
      177 m2
    • Wingspan (Beam)
      31 m
      47 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
      26403 kg
      39606 kg
    • Max. takeoff weight (Gross weight)
      51890 kg
      77837 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
      84 per.
      126 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      522 km/h
      784 km/h
    • Сruise Speed
      462 km/h
      694 km/h
    • Stall Speed
      124 km/h
      188 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
      10880 hp
      16320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6925 m
      10388 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7209 km
      10815 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
      274 qt
      412 qt
    • Price
      41 USD
      750000000 USD

Douglas DC-7

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
34.2
88.7
Height (m)
0.6
 
9.7
50.1
Wings
Wing area (m2)
1.1
 
146.8
925
Wingspan (Beam) (m)
0.1
 
38.9
95
Weights
Empty weight (kg)
8
 
33,004.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
64,863.7
575,000
Capacity
Crew (per.)
1
 
5
112
2 Pilots, 1 Flight Engineer, 4 Flight attendants
Capacity passengers (per.)
1
 
105
400
Speeds
Max. Speed (km/h)
25
 
653
28,165
Сruise Speed (km/h)
52
 
578
3,087
Stall Speed (km/h)
40
 
156
257.7
Power
Total Power (hp)
0.4
 
13,600
60,000
4 powerplants 3400 hp each
Performance
Service ceiling (m)
0.6
 
8,656.3
161,544
Range (Ferry range) (km)
4
 
9,012
40,700
Stat
Number built (qt)
0
 
343
43,000
Introduction 1953
First flight 18.05.1953

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