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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      67 m2
      101 m2
    • Wingspan (Beam)
      18 m
      29 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
      3648 kg
      5472 kg
    • Max. takeoff weight (Gross weight)
      5536 kg
      8304 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      162 km/h
      244 km/h
    • Max. Speed
      148 km/h
      224 km/h
    • Сruise Speed
      142 km/h
      214 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
      1088 hp
      1632 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2680 m
      4020 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      849 km
      1275 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
      114 m/min
      172 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
      3 qt
      5 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-8

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17.0
88.7
Height (m)
0.6
 
5.7
50.1
Wings
Wing area (m2)
1.1
 
84.0
925
Wingspan (Beam) (m)
0.1
 
23.7
95
Weights
Empty weight (kg)
8
 
4,560
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,920
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
203
1,500
Max. Speed (km/h)
25
 
186
28,165
Сruise Speed (km/h)
52
 
178
3,087
Power
Total Power (hp)
0.4
 
1,360
60,000
2 powerplant
Performance
Service ceiling (m)
0.6
 
3,350
161,544
Range (Ferry range) (km)
4
 
1,062
40,700
Endurance (h)
0.0
 
5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
143
36,000
Combat
Guns (qt)
1
 
4
18
Stat
Number built (qt)
0
 
1
43,000
Introduction 1931
First flight 30.01.1931

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