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    • Year
      1906
      2018
    • Length
      33 m
      51 m
    • Height
      8 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 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
      54400 kg
      81600 kg
    • Max. takeoff weight (Gross weight)
      99200 kg
      148800 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
      55 qt
      83 qt
    • Ground Speed
      840 km/h
      1260 km/h
    • Max. Speed
      1840 km/h
      2760 km/h
    • Сruise Speed
      744 km/h
      1116 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      396 kN
      595 kN
    • Service ceiling
      10640 m
      15960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5440 km
      8160 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      1600 m
      2400 m
    • Landing roll
      960 m
      1440 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      720 m/min
      1080 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
      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
      397 qt
      597 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-22M

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
42.4
88.7
Height (m)
0.6
 
11.1
50.1
Wings
Wingspan (Beam) (m)
0.1
 
34.3
95
20° sweep
0.1
 
23.3
95
65° sweep
Weights
Empty weight (kg)
8
 
68,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
124,000
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, co-pilot, navigator, weapon systems operator
Hardpoints (qt)
1
 
3
2,576
Raduga Kh-22 missiles in weapons bay and on wing pylons or
1
 
10
2,576
6 × Raduga Kh-15 missiles on a MKU-6-1 rotary launcher in its bomb bay, plus 4 × Raduga Kh-15 missiles on two underwing pylons
1
 
69
2,576
69 × FAB-250 or 8 × FAB-1500 might be typical
Speeds
Ground Speed (km/h)
96.6
 
1,050
1,500
Max. Speed (km/h)
25
 
2,300
28,165
Сruise Speed (km/h)
52
 
930
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Thrust (kN)
1.5
 
495.8
1,914
2 powerplants 247,9 kN each
Performance
Service ceiling (m)
0.6
 
13,300
161,544
Range (Ferry range) (km)
4
 
6,800
40,700
Takeoff roll (m)
20
 
2,000
3,200
2000—2100 m
Landing roll (m)
20
 
1,200
2,570
1200—1300 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
900
36,000
Combat
Guns (qt)
1
 
1
18
23-mm GSh-23 cannon
Stat
Number built (qt)
0
 
497
43,000
Introduction 1972
First flight 30.08.1969

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