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    • Year
      1906
      2018
    • Length
      17 m
      27 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      53 m2
      81 m2
    • Wingspan (Beam)
      17 m
      27 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
      11944 kg
      17916 kg
    • Max. takeoff weight (Gross weight)
      20280 kg
      30420 kg
    • Loaded weight
      16744 kg
      25116 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
      640 km/h
      960 km/h
    • Max. Speed
      678 km/h
      1018 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
      3492 l
      5238 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      21 kN
      32 kN
    • Service ceiling
      8960 m
      13440 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2344 km
      3516 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      960 km
      1440 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
      120 qt
      180 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-78

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
22.0
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
67.4
925
Wingspan (Beam) (m)
0.1
 
21.7
95
Weights
Empty weight (kg)
8
 
14,930
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
25,350
575,000
Loaded weight (kg)
5
 
20,930
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
800
1,500
Max. Speed (km/h)
25
 
848
28,165
Fuel
Fuel Capacity (l)
23
 
4,365
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
26.5
1,914
Performance
Service ceiling (m)
0.6
 
11,200
161,544
Range (Ferry range) (km)
4
 
2,930
40,700
Сombat radius (km)
277
 
1,200
7,210
Stat
Number built (qt)
0
 
150
43,000
Introduction 1952
First flight 13.10.1949
Stop production 1959

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