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    • Year
      1906
      2018
    • Length
      43 m
      65 m
    • Height
      12 m
      19 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      248 m2
      374 m2
    • Wingspan (Beam)
      40 m
      62 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
      70560 kg
      105840 kg
    • Max. takeoff weight (Gross weight)
      143200 kg
      214800 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      24000 kg
      36001 kg
    • Payload
      24000 kg
      36001 kg
    • Capacity passengers
      176 per.
      264 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      696 km/h
      1044 km/h
    • Сruise Speed
      616 km/h
      924 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
      48000 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7776 km
      11664 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      1280 m
      1920 m
    • Landing roll
      1240 m
      1860 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
      25 qt
      39 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-114

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
54.1
88.7
Height (m)
0.6
 
15.5
50.1
Wings
Wing area (m2)
1.1
 
311.1
925
Wingspan (Beam) (m)
0.1
 
51.1
95
Weights
Empty weight (kg)
8
 
88,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
179,000
575,000
Capacity
Crew (per.)
1
 
5
112
Useful load (kg)
26.4
 
30,000.6
90,700
Payload (kg)
23
 
30,000.6
122,470
Capacity passengers (per.)
1
 
220
400
Speeds
Max. Speed (km/h)
25
 
870
28,165
at 7100 m
Сruise Speed (km/h)
52
 
770
3,087
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
 
9,720
40,700
loaded with 15000 kg
Takeoff roll (m)
20
 
1,600
3,200
Landing roll (m)
20
 
1,550
2,570
Stat
Number built (qt)
0
 
32
43,000
Introduction 1957
First flight 15.11.1957
Stop production 1991

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