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    • Year
      1906
      2018
    • Length
      26 m
      41 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      131 m2
      198 m2
    • Wingspan (Beam)
      34 m
      52 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
      30299 kg
      45450 kg
    • Max. takeoff weight (Gross weight)
      53705 kg
      80559 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      91 per.
      137 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      482 km/h
      724 km/h
    • Сruise Speed
      386 km/h
      580 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
      11200 hp
      16800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7802 m
      11705 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5408 km
      8112 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
      44 qt
      68 qt
    • Price
      980000 USD
      1470000 USD

Boeing 377 Stratocruiser

TypeAircraft
Company

Boeing

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
33.6
88.7
Height (m)
0.6
 
11.7
50.1
Wings
Wing area (m2)
1.1
 
164.3
925
Wingspan (Beam) (m)
0.1
 
43.1
95
Weights
Empty weight (kg)
8
 
37,875.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
67,131.7
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
114
400
Up to 100 passengers on main deck plus 14 in lower deck lounge
Speeds
Max. Speed (km/h)
25
 
603
28,165
Сruise Speed (km/h)
52
 
483
3,087
Power
Total Power (hp)
0.4
 
14,000
60,000
4 powerplants 3500 hp each
Performance
Service ceiling (m)
0.6
 
9,753.6
161,544
Range (Ferry range) (km)
4
 
6,760
40,700
Stat
Number built (qt)
0
 
56
43,000
Price (USD)
41.5
 
1.2 million
750.0 million
Introduction 1944
First flight 08.07.1947
Stop production 1963

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