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    • Year
      1906
      2018
    • Length
      45 m
      68 m
    • Height
      12 m
      20 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      248 m2
      374 m2
    • Wingspan (Beam)
      41 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
      6 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
      82400 kg
      123600 kg
    • Max. takeoff weight (Gross weight)
      140000 kg
      210000 kg
    • Loaded weight
      136800 kg
      205200 kg
    • Crew
      19 per.
      29 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
      632 km/h
      948 km/h
    • Сruise Speed
      416 km/h
      624 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
      67461 l
      101193 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      47200 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8560 m
      12840 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5600 km
      8400 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      16 h
      24 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
      6 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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-126

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
56.5
88.7
Height (m)
0.6
 
16.1
50.1
Wings
Wing area (m2)
1.1
 
311.1
925
Wingspan (Beam) (m)
0.1
 
51.4
95
Rotors
Rotor number (qt)
1
 
8
8
Weights
Empty weight (kg)
8
 
103,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
175,000
575,000
Loaded weight (kg)
5
 
171,000
242,500
Capacity
Crew (per.)
1
 
24
112
12 + full spare crew
Speeds
Max. Speed (km/h)
25
 
790
28,165
Сruise Speed (km/h)
52
 
520
3,087
Fuel
Fuel Capacity (l)
23
 
84,327.3
320,000
Power
Power/mass (hp/kg)
0.0
 
0.4
22.1
Total Power (hp)
0.4
 
59,000
60,000
4 powerplants 14795 hp each
Performance
Service ceiling (m)
0.6
 
10,700
161,544
Range (Ferry range) (km)
4
 
7,000
40,700
with internal fuel only
Endurance (h)
0.0
 
20
150
with 1 in-flight refuel
Propellers
Prop blade number (qt)
1
 
8
8
Stat
Number built (qt)
0
 
12
43,000
Introduction 1962
First flight 23.01.1962
Stop production 1984

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