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    • Year
      1906
      2018
    • Length
      56 m
      85 m
    • Height
      15 m
      24 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      408 m2
      614 m2
    • Wingspan (Beam)
      47 m
      72 m
    • Wing loading
      584 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
      152000 kg
      228000 kg
    • Max. takeoff weight (Gross weight)
      302273 kg
      453411 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      89 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      775 km/h
      1163 km/h
    • Сruise Speed
      716 km/h
      1074 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
      150395 l
      225593 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      748 kN
      1124 kN
    • Service ceiling
      11200 m
      16800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      9185 km
      13779 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      120 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
      3 qt
      5 qt
    • Price
      178400000 USD
      267600000 USD

Boeing E-4

TypeAircraft
Company

Boeing

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
70.5
88.7
Height (m)
0.6
 
19.3
50.1
Wings
Wing area (m2)
1.1
 
511.0
925
Wingspan (Beam) (m)
0.1
 
59.7
95
Wing loading (kg/m2)
3.1
 
730
829
Weights
Empty weight (kg)
8
 
190,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
377,842.4
575,000
Capacity
Crew (per.)
1
 
112
112
including flight and mission personnel
Speeds
Max. Speed (km/h)
25
 
969
28,165
Сruise Speed (km/h)
52
 
895
3,087
Fuel
Fuel Capacity (l)
23
 
187,993.8
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
936
1,914
4 powerplants 234 kN powerplants each
Performance
Service ceiling (m)
0.6
 
14,000
161,544
Range (Ferry range) (km)
4
 
11,482.4
40,700
Endurance (h)
0.0
 
150
150
or more
Stat
Number built (qt)
0
 
4
43,000
Price (USD)
41.5
 
223.0 million
750.0 million
Introduction 1974

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