Search filter

    • Year
      1906
      2018
    • Length
      70 m
      89 m
    • Height
      13 m
      21 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      43 m
      66 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
      137600 kg
      206400 kg
    • Max. takeoff weight (Gross weight)
      280000 kg
      420000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      256 per.
      384 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      1740 km/h
      2610 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
      1 kN
      1914 kN
    • Service ceiling
      16000 m
      24000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7360 km
      11040 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-244

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Integrated

Concept

Monoplane

Geometry
Length (m)
1.9
 
88.7
88.7
Height (m)
0.6
 
16.9
50.1
from ground to the top of the tail fin
Wings
Wingspan (Beam) (m)
0.1
 
54.8
95
Weights
Empty weight (kg)
8
 
172,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
350,000
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
320
400
or 250 passengers depending on the project
Speeds
Сruise Speed (km/h)
52
 
2,175
3,087
Performance
Service ceiling (m)
0.6
 
20,000
161,544
Range (Ferry range) (km)
4
 
9,200
40,700
fully loaded; according to other sources 7500 km
Stat
Introduction 1999

Similar aircraft

Get more

Comments