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    • Year
      1906
      2018
    • Length
      43 m
      65 m
    • Height
      10 m
      16 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      288 m2
      432 m2
    • Wingspan (Beam)
      26 m
      41 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
      88000 kg
      132000 kg
    • Max. takeoff weight (Gross weight)
      220000 kg
      330000 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      824 km/h
      1236 km/h
    • Max. Speed
      1776 km/h
      2664 km/h
    • Сruise Speed
      768 km/h
      1152 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
      1 kN/kg
    • Afterburning thrust
      784 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      439 kN
      660 kN
    • Service ceiling
      12004 m
      18008 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      9840 km
      14760 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      12 h
      18 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      3 G
    • Rate of climb
      3360 m/min
      5040 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
      19 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
      28 qt
      42 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-160

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Integrated

Geometry
Length (m)
1.9
 
54.1
88.7
Height (m)
0.6
 
13.1
50.1
Wings
Wing area (m2)
1.1
 
360
925
Wingspan (Beam) (m)
0.1
 
55.7
95
20° sweep
0.1
 
33.6
95
65° sweep
Weights
Empty weight (kg)
8
 
110,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
275,000
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, co-pilot, bombardier, defensive systems operator
Speeds
Ground Speed (km/h)
96.6
 
1,030
1,500
Max. Speed (km/h)
25
 
2,220
28,165
at 12200 m
Сruise Speed (km/h)
52
 
960
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Afterburning thrust (kN/kg)
29.4
 
980
980
245 kN each
Thrust (kN)
1.5
 
549.2
1,914
4 powerplants 137,3 kN each
Performance
Service ceiling (m)
0.6
 
15,006
161,544
Range (Ferry range) (km)
4
 
12,300
40,700
without in-flight refuelling and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves
Endurance (h)
0.0
 
15
150
Dynamic Performance
Load factor from (G)
2
 
2
9
Rate of climb (m/min)
1.9
 
4,200
36,000
Combat
Missiles (qt)
1
 
12
24
Two internal rotary launchers each holding 6× Raduga Kh-55SM/101/102/555 cruise missiles or
1
 
24
24
Two internal rotary launchers each holding 12× AS-16 Kickback short-range nuclear missiles
Stat
Number built (qt)
0
 
35
43,000
Introduction 1981
First flight 19.12.1981

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