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    • Year
      1906
      2018
    • Length
      30 m
      47 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      139 m2
      210 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
      34400 kg
      51600 kg
    • Max. takeoff weight (Gross weight)
      60800 kg
      91200 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 per.
    • Useful load
      8000 kg
      12000 kg
    • Payload
      8000 kg
      12000 kg
    • Capacity passengers
      56 per.
      84 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      760 km/h
      1140 km/h
    • Сruise Speed
      620 km/h
      930 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
      149 kN
      224 kN
    • Service ceiling
      9400 m
      14100 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2640 km
      3960 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      1576 m
      2364 m
    • Landing roll
      1480 m
      2220 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
      3 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-107

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
38.6
88.7
Height (m)
0.6
 
11.5
50.1
Wings
Wing area (m2)
1.1
 
174.5
925
Wingspan (Beam) (m)
0.1
 
34.5
95
Weights
Empty weight (kg)
8
 
43,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
76,000
575,000
Capacity
Crew (per.)
1
 
6
112
Useful load (kg)
26.4
 
10,000
90,700
Payload (kg)
23
 
10,000
122,470
Capacity passengers (per.)
1
 
70
400
Speeds
Max. Speed (km/h)
25
 
950
28,165
Сruise Speed (km/h)
52
 
775
3,087
Power
Thrust (kN)
1.5
 
186.4
1,914
2 powerplants 93,2 kW each
Performance
Service ceiling (m)
0.6
 
11,750
161,544
Range (Ferry range) (km)
4
 
3,300
40,700
with 10,000 kg payload, 775 km/h at 10,000 m
Takeoff roll (m)
20
 
1,970
3,200
Landing roll (m)
20
 
1,850
2,570
Combat
Guns (qt)
1
 
2
18
23mm Afanasev Makarov AM-23 cannon
Stat
Number built (qt)
0
 
1
43,000
Introduction 1958
First flight 1958

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