Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      150 m2
      227 m2
    • Wingspan (Beam)
      31 m
      47 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
      14856 kg
      22286 kg
    • Max. takeoff weight (Gross weight)
      28000 kg
      42000 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      8 per.
      14 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
      277 km/h
      417 km/h
    • Max. Speed
      354 km/h
      532 km/h
    • Сruise Speed
      52 km/h
      3087 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
      4288 hp
      6432 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7440 m
      11160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2960 km
      4440 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
      283 m/min
      425 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
      74 qt
      112 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-42

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
23.2
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
188.7
925
Wingspan (Beam) (m)
0.1
 
39.1
95
Weights
Empty weight (kg)
8
 
18,571
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
35,000
575,000
Capacity
Crew (per.)
1
 
11
112
8 - 12 persons
Speeds
Ground Speed (km/h)
96.6
 
347
1,500
Max. Speed (km/h)
25
 
443
28,165
on 6360 m
Power
Total Power (hp)
0.4
 
5,360
60,000
Performance
Service ceiling (m)
0.6
 
9,300
161,544
Range (Ferry range) (km)
4
 
3,700
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
354
36,000
Stat
Number built (qt)
0
 
93
43,000
including 2 prototypes
Introduction 1936
First flight 27.12.1936

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