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    • Year
      1906
      2018
    • Length
      36 m
      56 m
    • Height
      12 m
      19 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      248 m2
      374 m2
    • Wingspan (Beam)
      43 m
      65 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
      74800 kg
      112200 kg
    • Max. takeoff weight (Gross weight)
      145600 kg
      218400 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      5 per.
      9 per.
    • Useful load
      25546 kg
      38320 kg
    • Payload
      25546 kg
      38320 kg
    • Capacity passengers
      19 per.
      29 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      720 km/h
      1080 km/h
    • Сruise Speed
      640 km/h
      960 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
      62240 l
      93360 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
      48000 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      8600 km
      12900 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-116

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
46.2
88.7
Height (m)
0.6
 
15.5
50.1
Wings
Wing area (m2)
1.1
 
311.1
925
Wingspan (Beam) (m)
0.1
 
54.1
95
Weights
Empty weight (kg)
8
 
93,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
182,000
575,000
Capacity
Crew (per.)
1
 
7
112
or 8
Useful load (kg)
26.4
 
31,932.9
90,700
Payload (kg)
23
 
31,932.9
122,470
Capacity passengers (per.)
1
 
24
400
max. 60 passengers
Speeds
Max. Speed (km/h)
25
 
900
28,165
Сruise Speed (km/h)
52
 
800
3,087
Fuel
Fuel Capacity (l)
23
 
77,800
320,000
Power
Total Power (hp)
0.4
 
60,000
60,000
4 powerplants 15000 hp each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
10,750
40,700
Stat
Number built (qt)
0
 
2
43,000
Introduction 1957
First flight 1957

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