Search filter

    • Year
      1906
      2018
    • Length
      24 m
      37 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      95 m2
      144 m2
    • Wingspan (Beam)
      20 m
      31 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
      18320 kg
      27480 kg
    • Max. takeoff weight (Gross weight)
      30000 kg
      45000 kg
    • Loaded weight
      24000 kg
      36000 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      44 per.
      68 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      776 km/h
      1164 km/h
    • Сruise Speed
      696 km/h
      1044 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
      84 kN
      128 kN
    • Service ceiling
      9360 m
      14040 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1680 km
      2520 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
      576 m/min
      864 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
      131 qt
      197 qt
    • Price
      41 USD
      750000000 USD

Tupolev 127

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
30.6
88.7
Height (m)
0.6
 
8.1
50.1
Wings
Wing area (m2)
1.1
 
119.4
925
Wingspan (Beam) (m)
0.1
 
25.6
95
Weights
Empty weight (kg)
8
 
22,900
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
37,500
575,000
Loaded weight (kg)
5
 
30,000
242,500
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
56
400
Speeds
Max. Speed (km/h)
25
 
970
28,165
at 8000 m
Сruise Speed (km/h)
52
 
870
3,087
800-870 km/h
Power
Thrust (kN)
1.5
 
106.2
1,914
2 powerplants 53.1 kN each
Performance
Service ceiling (m)
0.6
 
11,700
161,544
Range (Ferry range) (km)
4
 
2,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
720
36,000
Stat
Number built (qt)
0
 
164
43,000
Introduction 1960
First flight 29.03.1960
Stop production 1980

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