Search filter

    • Year
      1906
      2018
    • Length
      26 m
      40 m
    • Height
      27 m
      41 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      388 m2
      584 m2
    • Wingspan (Beam)
      50 m
      76 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
      22800 kg
      34200 kg
    • Max. takeoff weight (Gross weight)
      42400 kg
      63600 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      16 per.
      24 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      48 per.
      72 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      176 km/h
      264 km/h
    • Сruise Speed
      158 km/h
      238 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
      5720 l
      8580 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
      5760 hp
      8640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3600 m
      5400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      960 km
      1440 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-20bis

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
32.9
88.7
Height (m)
0.6
 
34
50.1
Wings
Wing area (m2)
1.1
 
486
925
Wingspan (Beam) (m)
0.1
 
63
95
Weights
Empty weight (kg)
8
 
28,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
53,000
575,000
Capacity
Crew (per.)
1
 
20
112
Capacity passengers (per.)
1
 
60
400
Speeds
Max. Speed (km/h)
25
 
220
28,165
Сruise Speed (km/h)
52
 
198
3,087
Fuel
Fuel Capacity (l)
23
 
7,150
320,000
Power
Total Power (hp)
0.4
 
7,200
60,000
8 powerplants
Performance
Service ceiling (m)
0.6
 
4,500
161,544
Range (Ferry range) (km)
4
 
1,200
40,700
Stat
Number built (qt)
0
 
2
43,000
Introduction 1934
First flight 19.05.1934
Stop production 1942

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