Search filter

    • Year
      1906
      2018
    • Length
      28 m
      44 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      108 m2
      164 m2
    • Wingspan (Beam)
      12 m
      20 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
      15440 kg
      23160 kg
    • Max. takeoff weight (Gross weight)
      32800 kg
      49200 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
      840 km/h
      1260 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
      152 kN
      228 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      6000 km
      9000 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 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
      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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-444

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Integrated

Concept

Monoplane

Geometry
Length (m)
1.9
 
36
88.7
Height (m)
0.6
 
6.5
50.1
Wings
Wing area (m2)
1.1
 
136
925
Wingspan (Beam) (m)
0.1
 
16.2
95
Weights
Empty weight (kg)
8
 
19,300
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
41,000
575,000
Speeds
Сruise Speed (km/h)
52
 
2,125
3,087
supersonic
52
 
1,050
3,087
subsonic
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Thrust (kN)
1.5
 
190
1,914
2 powerplants 95 kN each
Performance
Range (Ferry range) (km)
4
 
7,500
40,700
Stat

Similar aircraft

Get more

Comments