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    • Year
      1906
      2018
    • Length
      31 m
      48 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      218 m2
      329 m2
    • Wingspan (Beam)
      44 m
      68 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
      43768 kg
      65654 kg
    • Max. takeoff weight (Gross weight)
      85833 kg
      128751 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
      367 km/h
      551 km/h
    • Max. Speed
      510 km/h
      766 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
      50880 l
      76320 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
      13760 hp
      20640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9360 m
      14040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      9600 km
      14400 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      1312 m
      1968 m
    • Landing roll
      1200 m
      1800 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      816 m/min
      1224 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      7 min
      11 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      8 qt
      12 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      14400 kg
      21600 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-85

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
39.3
88.7
Height (m)
0.6
 
11.4
50.1
Wings
Wing area (m2)
1.1
 
273.6
925
Wingspan (Beam) (m)
0.1
 
56.0
95
Weights
Empty weight (kg)
8
 
54,711
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
107,292
575,000
Capacity
Crew (per.)
1
 
11
112
or 12
Speeds
Ground Speed (km/h)
96.6
 
459
1,500
Max. Speed (km/h)
25
 
638
28,165
at 10000 m
Fuel
Fuel Capacity (l)
23
 
63,600
320,000
Power
Total Power (hp)
0.4
 
17,200
60,000
4 powerplants 4300 hp each
Performance
Service ceiling (m)
0.6
 
11,700
161,544
Range (Ferry range) (km)
4
 
12,000
40,700
Takeoff roll (m)
20
 
1,640
3,200
Landing roll (m)
20
 
1,500
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,020
36,000
Time to altitude (min)
0.6
 
8.9
105
to 5000 m
Combat
Guns (qt)
1
 
10
18
23 mm Nudelman NR-23 cannons
Bombs weight (kg)
2
 
18,000
39,000
of bombs
Stat
Number built (qt)
0
 
2
43,000
Introduction 1951
First flight 09.01.1951

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