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    • Year
      1906
      2018
    • Length
      37 m
      56 m
    • Height
      10 m
      16 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      35 m
      54 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
      53124 kg
      79688 kg
    • Max. takeoff weight (Gross weight)
      121056 kg
      181584 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      151 per.
      227 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      777 km/h
      1167 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
      72128 l
      108192 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
      0 hp
      60000 hp
    • Thrust
      270 kN
      406 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5536 km
      8304 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
      1450 m
      2176 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
      123 qt
      185 qt
    • Price
      41 USD
      750000000 USD

Boeing 720

Company

Boeing

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
46.6
88.7
41,25 m - 46,61 m depending on variant
Height (m)
0.6
 
12.9
50.1
or 12,65 depending on variant
Wings
Wingspan (Beam) (m)
0.1
 
44.4
95
or 39,9 depending on variant
Weights
Empty weight (kg)
8
 
66,406
276,800
46785 kg - 66406 kg depending on variant
Max. takeoff weight (Gross weight) (kg)
154
 
151,320
575,000
100800 kg - 151320 kg depending on variant
Capacity
Crew (per.)
1
 
4
112
Pilot, Co-Pilot, Flight Engineer, Navigator
Capacity passengers (per.)
1
 
189
400
110-189 depending on variant
Speeds
Сruise Speed (km/h)
52
 
972
3,087
or 1000 km/h depending on variant
Fuel
Fuel Capacity (l)
23
 
90,160
320,000
60900 l - 90160 l depending on variant
Power
Thrust (kN)
1.5
 
337.6
1,914
4 powerplants 84,4 kN each (or 53,3 kN, or 75,6 kN depending
Performance
Range (Ferry range) (km)
4
 
6,920
40,700
or 6820 km depending on variant (max. payload)
Landing roll (m)
20
 
1,813
2,570
1740 m - 1813 m depending on variant
Stat
Number built (qt)
0
 
154
43,000
First flight 23.11.1959
Stop production 29.09.2010

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