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    • Year
      1906
      2018
    • Length
      25 m
      39 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      213 m2
      320 m2
    • Wingspan (Beam)
      37 m
      56 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
      17563 kg
      26345 kg
    • Max. takeoff weight (Gross weight)
      29936 kg
      44906 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      14 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      3628 kg
      5444 kg
    • Capacity passengers
      59 per.
      89 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      272 km/h
      408 km/h
    • Сruise Speed
      241 km/h
      363 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
      5120 hp
      7680 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4779 m
      7169 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4716 km
      7076 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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

Boeing 314 Clipper

TypeAircraft
Company

Boeing

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
32.3
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
266.3
925
Wingspan (Beam) (m)
0.1
 
46.4
95
Weights
Empty weight (kg)
8
 
21,953.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,421
575,000
Capacity
Crew (per.)
1
 
11
112
including 2 cabin stewards
Payload (kg)
23
 
4,535.9
122,470
of mail and cargo
Capacity passengers (per.)
1
 
74
400
Daytime: 74 passengers, Nighttime: 36 passengers
Speeds
Max. Speed (km/h)
25
 
340
28,165
Сruise Speed (km/h)
52
 
302
3,087
at 3400 m
Power
Total Power (hp)
0.4
 
6,400
60,000
4 powerplants 1600 hp each
Performance
Service ceiling (m)
0.6
 
5,974.1
161,544
Range (Ferry range) (km)
4
 
5,896
40,700
Stat
Number built (qt)
0
 
12
43,000
Introduction 1939
First flight 07.06.1938
Stop production 1946

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