Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      46 m2
      70 m2
    • Wingspan (Beam)
      16 m
      25 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
      4368 kg
      6552 kg
    • Max. takeoff weight (Gross weight)
      5896 kg
      8844 kg
    • Loaded weight
      5 kg
      242500 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
      297 km/h
      447 km/h
    • Сruise Speed
      246 km/h
      370 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
      1000 l
      1500 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
      800 hp
      1200 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5360 m
      8040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1312 km
      1968 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
      1 m/min
      36000 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
      8 qt
      14 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-35

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
15.4
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
57.8
925
Wingspan (Beam) (m)
0.1
 
20.8
95
Weights
Empty weight (kg)
8
 
5,460
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,370
575,000
Capacity
Crew (per.)
1
 
2
112
or 3
Speeds
Max. Speed (km/h)
25
 
372
28,165
Сruise Speed (km/h)
52
 
308
3,087
Fuel
Fuel Capacity (l)
23
 
1,250
320,000
Power
Total Power (hp)
0.4
 
1,000
60,000
Performance
Service ceiling (m)
0.6
 
6,700
161,544
Range (Ferry range) (km)
4
 
1,640
40,700
Stat
Number built (qt)
0
 
11
43,000
Introduction 1936
First flight 1936

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