Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      9 m
      14 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
      936 kg
      1404 kg
    • Max. takeoff weight (Gross weight)
      1232 kg
      1848 kg
    • Loaded weight
      1232 kg
      1848 kg
    • Crew
      1 per.
      2 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
      285 km/h
      429 km/h
    • Max. Speed
      359 km/h
      539 km/h
    • Сruise Speed
      274 km/h
      412 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
      600 hp
      900 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7544 m
      11316 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      480 km
      720 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
      615 m/min
      923 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      8 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 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
      16 qt
      24 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-31

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
6.1
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
16.9
925
Wingspan (Beam) (m)
0.1
 
11.3
95
Weights
Empty weight (kg)
8
 
1,170
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,540
575,000
Loaded weight (kg)
5
 
1,540
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
357
1,500
Max. Speed (km/h)
25
 
449
28,165
Сruise Speed (km/h)
52
 
343
3,087
Power
Total Power (hp)
0.4
 
750
60,000
Performance
Service ceiling (m)
0.6
 
9,430
161,544
Range (Ferry range) (km)
4
 
600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
769
36,000
Time to altitude (min)
0.6
 
6.5
105
Combat
Guns (qt)
1
 
2
18
Stat
Number built (qt)
0
 
20
43,000
Introduction 1933
First flight 27.05.1933

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