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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      25 m2
    • Wingspan (Beam)
      7 m
      11 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
      784 kg
      1176 kg
    • Max. takeoff weight (Gross weight)
      1139 kg
      1709 kg
    • Loaded weight
      5 kg
      242500 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
      242 km/h
      364 km/h
    • Max. Speed
      250 km/h
      376 km/h
    • Сruise Speed
      229 km/h
      345 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
      560 hp
      840 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6800 m
      10200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      352 km
      528 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
      666 m/min
      1000 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
      2 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-13

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.7
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
20.3
925
Wingspan (Beam) (m)
0.1
 
9.0
95
Weights
Empty weight (kg)
8
 
980
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,424
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
303
1,500
Max. Speed (km/h)
25
 
313
28,165
Сruise Speed (km/h)
52
 
287
3,087
Power
Total Power (hp)
0.4
 
700
60,000
Performance
Service ceiling (m)
0.6
 
8,500
161,544
Range (Ferry range) (km)
4
 
440
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
833
36,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1930
First flight 12.12.1930

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