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    • Year
      1906
      2018
    • Length
      32 m
      49 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      148 m2
      224 m2
    • Wingspan (Beam)
      27 m
      42 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
      33280 kg
      49920 kg
    • Max. takeoff weight (Gross weight)
      60800 kg
      91200 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      5 per.
      9 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      92 per.
      138 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      760 km/h
      1142 km/h
    • Сruise Speed
      640 km/h
      960 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
      0 hp
      60000 hp
    • Thrust
      152 kN
      229 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2200 km
      3300 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
      480 m/min
      720 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
      160 qt
      242 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-104

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
40.1
88.7
Height (m)
0.6
 
11.9
50.1
Wings
Wing area (m2)
1.1
 
186.1
925
Wingspan (Beam) (m)
0.1
 
34.5
95
Weights
Empty weight (kg)
8
 
43,800
276,800
8
 
41,600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
76,000
575,000
154
 
76,000
575,000
Capacity
Crew (per.)
1
 
7
112
Capacity passengers (per.)
1
 
115
400
Speeds
Max. Speed (km/h)
25
 
951
28,165
Сruise Speed (km/h)
52
 
800
3,087
Power
Thrust (kN)
1.5
 
190.2
1,914
2 powerplants 95,1 kN each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
2,750
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
600
36,000
Stat
Number built (qt)
0
 
201
43,000
Introduction 1963
First flight 17.06.1955
Stop production 1986

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