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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      90 m2
      137 m2
    • Wingspan (Beam)
      19 m
      30 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
      3839 kg
      5760 kg
    • Max. takeoff weight (Gross weight)
      6350 kg
      9526 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      325 kg
      489 kg
    • Capacity passengers
      14 per.
      22 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      177 km/h
      267 km/h
    • Сruise Speed
      160 km/h
      242 km/h
    • Stall Speed
      71 km/h
      107 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
      1260 hp
      1890 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3413 m
      5121 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      592 km
      890 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
      219 m/min
      330 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
      12 qt
      20 qt
    • Price
      60000 USD
      90000 USD

Boeing 80

TypeAircraft
Company

Boeing

Scheme

Biplane

Geometry
Length (m)
1.9
 
17.2
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
113.3
925
Wingspan (Beam) (m)
0.1
 
24.4
95
Weights
Empty weight (kg)
8
 
4,799.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,937.9
575,000
Capacity
Crew (per.)
1
 
3
112
Payload (kg)
23
 
407.3
122,470
Capacity passengers (per.)
1
 
18
400
Speeds
Max. Speed (km/h)
25
 
222
28,165
Сruise Speed (km/h)
52
 
201
3,087
Stall Speed (km/h)
40
 
89
257.7
Power
Total Power (hp)
0.4
 
1,575
60,000
3 powerplants 525 hp each
Performance
Service ceiling (m)
0.6
 
4,267.2
161,544
Range (Ferry range) (km)
4
 
741
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
274.3
36,000
Stat
Number built (qt)
0
 
16
43,000
Price (USD)
41.5
 
75,000
750.0 million
Introduction 1928
First flight 27.07.1928
Stop production 1934

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