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    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      39 m2
      59 m2
    • Wingspan (Beam)
      12 m
      19 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
      1376 kg
      2064 kg
    • Max. takeoff weight (Gross weight)
      2136 kg
      3204 kg
    • Loaded weight
      2336 kg
      3504 kg
    • Crew
      1 per.
      3 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
      188 km/h
      282 km/h
    • Сruise Speed
      169 km/h
      255 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
      400 hp
      600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      880 km
      1320 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      6 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
      116 m/min
      174 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      2 min
      4 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-10

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.9
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
49
925
Wingspan (Beam) (m)
0.1
 
15.2
95
Weights
Empty weight (kg)
8
 
1,720
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,670
575,000
Loaded weight (kg)
5
 
2,920
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
235
28,165
Сruise Speed (km/h)
52
 
212
3,087
Power
Total Power (hp)
0.4
 
500
60,000
Performance
Service ceiling (m)
0.6
 
5,500
161,544
Range (Ferry range) (km)
4
 
1,100
40,700
Endurance (h)
0.0
 
5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
145
36,000
Time to altitude (min)
0.6
 
3.1
105
Combat
Guns (qt)
1
 
2
18
Stat
Number built (qt)
0
 
1
43,000
Introduction 1930
First flight 30.01.1930

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