Search filter

    • Year
      1906
      2018
    • Length
      28 m
      43 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      129 m2
      195 m2
    • Wingspan (Beam)
      35 m
      54 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
      30632 kg
      45948 kg
    • Max. takeoff weight (Gross weight)
      48000 kg
      72000 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
      57 per.
      87 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      454 km/h
      682 km/h
    • Сruise Speed
      450 km/h
      676 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
      7680 hp
      11520 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3920 km
      5880 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      536 m
      804 m
    • Landing roll
      480 m
      720 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
      16 min
      26 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Tupolev Tu-70

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
35.4
88.7
Height (m)
0.6
 
9.8
50.1
Wings
Wing area (m2)
1.1
 
161.7
925
Wingspan (Beam) (m)
0.1
 
44.3
95
Weights
Empty weight (kg)
8
 
38,290
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
60,000
575,000
Capacity
Crew (per.)
1
 
7
112
or 8
Capacity passengers (per.)
1
 
72
400
Up to 72
Speeds
Max. Speed (km/h)
25
 
568
28,165
at 9000 m
Сruise Speed (km/h)
52
 
563
3,087
Power
Total Power (hp)
0.4
 
9,600
60,000
4 powerplants 2400 hp each
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
4,900
40,700
Takeoff roll (m)
20
 
670
3,200
Landing roll (m)
20
 
600
2,570
Dynamic Performance
Time to altitude (min)
0.6
 
21.2
105
to 5000 m
Stat
Number built (qt)
0
 
1
43,000
Introduction 1946
First flight 27.11.1946

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