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    • Year
      1906
      2018
    • Length
      31 m
      47 m
    • Height
      8 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      603 m2
      905 m2
    • Wingspan (Beam)
      76 m
      95 m
    • Wing loading
      70 kg/m2
      106 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
      38880 kg
      58320 kg
    • Max. takeoff weight (Gross weight)
      60800 kg
      91200 kg
    • Loaded weight
      56800 kg
      85200 kg
    • Crew
      13 per.
      21 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
      220 km/h
      330 km/h
    • Max. Speed
      240 km/h
      360 km/h
    • Сruise Speed
      136 km/h
      204 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
      8000 l
      12000 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
      11520 hp
      17280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      104 m/min
      156 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-26

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Concept

Midwing

Geometry
Length (m)
1.9
 
39
88.7
Height (m)
0.6
 
10
50.1
Wings
Wing area (m2)
1.1
 
754
925
Wingspan (Beam) (m)
0.1
 
95
95
Wing loading (kg/m2)
3.1
 
88
829
Weights
Empty weight (kg)
8
 
48,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
76,000
575,000
Loaded weight (kg)
5
 
71,000
242,500
Capacity
Crew (per.)
1
 
17
112
Speeds
Ground Speed (km/h)
96.6
 
275
1,500
Max. Speed (km/h)
25
 
300
28,165
Сruise Speed (km/h)
52
 
170
3,087
Fuel
Fuel Capacity (l)
23
 
10,000
320,000
Power
Total Power (hp)
0.4
 
14,400
60,000
12 powerplants
Performance
Service ceiling (m)
0.6
 
5,500
161,544
lightly loaded
Range (Ferry range) (km)
4
 
1,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
130
36,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1936

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