Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      45 m2
      69 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
      3814 kg
      5722 kg
    • Max. takeoff weight (Gross weight)
      6304 kg
      9456 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
      288 km/h
      432 km/h
    • Max. Speed
      360 km/h
      540 km/h
    • Сruise Speed
      318 km/h
      478 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
      1536 hp
      2304 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7440 m
      11160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1840 km
      2760 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
      456 m/min
      684 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
      6 qt
      10 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
      5324 qt
      7988 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-46

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
12.6
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
56.7
925
Wingspan (Beam) (m)
0.1
 
20.3
95
Weights
Empty weight (kg)
8
 
4,768
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,880
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
360
1,500
Max. Speed (km/h)
25
 
450
28,165
at 4100 m
Сruise Speed (km/h)
52
 
398
3,087
Power
Total Power (hp)
0.4
 
1,920
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
9,300
161,544
Range (Ferry range) (km)
4
 
2,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
570
36,000
Combat
Guns (qt)
1
 
4
18
wo in nose, one in dorsal and one in ventral position
Bombs (qt)
1
 
8
250
6 × 100 kg (220 lb) or six 50 kg (110 lb) bombs in bomb-bay, 2 × 250 kg (550 lb) bombs on wing racks
Stat
Number built (qt)
0
 
6,656
43,000
Introduction 1939
First flight 07.10.1934
Stop production 1950

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