Search filter

    • Year
      1906
      2018
    • Length
      42 m
      64 m
    • Height
      11 m
      18 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      248 m2
      374 m2
    • Wingspan (Beam)
      40 m
      60 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
      74400 kg
      111600 kg
    • Max. takeoff weight (Gross weight)
      148000 kg
      222000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      12 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
      740 km/h
      1110 km/h
    • Сruise Speed
      568 km/h
      854 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
      87000 l
      130500 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
      10800 m
      16200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      10040 km
      15060 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      5120 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      2560 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
      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
      80 qt
      120 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-142

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
53.1
88.7
Height (m)
0.6
 
14.7
50.1
Wings
Wing area (m2)
1.1
 
311.1
925
Wingspan (Beam) (m)
0.1
 
50
95
Weights
Empty weight (kg)
8
 
93,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
185,000
575,000
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
925
28,165
Сruise Speed (km/h)
52
 
711
3,087
Fuel
Fuel Capacity (l)
23
 
108,750
320,000
Power
Total Power (hp)
0.4
 
60,000
60,000
4 powerplants 15000 hp each
Performance
Service ceiling (m)
0.6
 
13,500
161,544
Range (Ferry range) (km)
4
 
12,550
40,700
Сombat radius (km)
277
 
6,400
7,210
Takeoff roll (m)
20
 
3,200
3,200
Stat
Number built (qt)
0
 
100
43,000
Introduction 1968
First flight 18.07.1968

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