Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      2 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      2 m2
      4 m2
    • Wingspan (Beam)
      1 m
      3 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
      984 kg
      1476 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 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
      25 km/h
      28165 km/h
    • Сruise Speed
      760 km/h
      1140 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      5 kN
      8 kN
    • Service ceiling
      800 m
      1200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      160 km
      240 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      1 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
      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
      760 qt
      1140 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-143

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Unmanned

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
1.5
50.1
Wings
Wing area (m2)
1.1
 
2.9
925
Wingspan (Beam) (m)
0.1
 
2.2
95
Weights
Empty weight (kg)
8
 
1,230
276,800
Speeds
Сruise Speed (km/h)
52
 
950
3,087
Power
Thrust (kN)
1.5
 
6.3
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
1,000
161,544
Range (Ferry range) (km)
4
 
200
40,700
Endurance (h)
0.0
 
0.2
150
13 min
Stat
Number built (qt)
0
 
950
43,000
Introduction 1973
First flight 1970

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