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    • Year
      1906
      2018
    • Length
      33 m
      50 m
    • Height
      8 m
      13 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      129 m2
      195 m2
    • Wingspan (Beam)
      18 m
      28 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
      34864 kg
      52296 kg
    • Max. takeoff weight (Gross weight)
      73600 kg
      110400 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      1208 km/h
      1812 km/h
    • Сruise Speed
      680 km/h
      1020 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
      32640 l
      48960 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
      129 kN/kg
      195 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      172 kN
      259 kN
    • Service ceiling
      10640 m
      15960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3920 km
      5880 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2520 km
      3780 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      2 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
      248 qt
      374 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-22

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
41.6
88.7
Height (m)
0.6
 
10.1
50.1
Wings
Wing area (m2)
1.1
 
162.3
925
Wingspan (Beam) (m)
0.1
 
23.2
95
Weights
Empty weight (kg)
8
 
43,580
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
92,000
575,000
Capacity
Crew (per.)
1
 
3
112
pilot, navigator, weapons officer
Speeds
Max. Speed (km/h)
25
 
1,510
28,165
Сruise Speed (km/h)
52
 
850
3,087
Fuel
Fuel Capacity (l)
23
 
40,800
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Afterburning thrust (kN/kg)
29.4
 
161.9
980
2 powerplants 161,9 kN each
Thrust (kN)
1.5
 
215.8
1,914
107,9 kN each
Performance
Service ceiling (m)
0.6
 
13,300
161,544
Range (Ferry range) (km)
4
 
4,900
40,700
Сombat radius (km)
277
 
3,150
7,210
Combat
Guns (qt)
1
 
1
18
R-23 23 mm cannon
Missiles (qt)
1
 
1
24
Kh-22 (AS-4 Kitchen) cruise missile
Stat
Number built (qt)
0
 
311
43,000
Introduction 1962
First flight 07.09.1959
Stop production 1998

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