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    • Year
      1906
      2018
    • Length
      24 m
      37 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      129 m2
      195 m2
    • Wingspan (Beam)
      34 m
      52 m
    • Wing loading
      320 kg/m2
      480 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      9
      14
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      3 qt
      5 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
      29480 kg
      44220 kg
    • Max. takeoff weight (Gross weight)
      50880 kg
      76320 kg
    • Loaded weight
      38280 kg
      57420 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
      96 km/h
      1500 km/h
    • Max. Speed
      446 km/h
      670 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
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 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
      8960 m
      13440 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      768 m
      1152 m
    • Landing roll
      736 m
      1104 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      220 m/min
      332 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      14 min
      22 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      4 m
      6 m
    • Prop blade number
      3 qt
      5 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
      677 qt
      1017 qt
    • Price
      41 USD
      750000000 USD

Tupolev 94

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
30.2
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wing area (m2)
1.1
 
161.7
925
Wingspan (Beam) (m)
0.1
 
43.1
95
Wing loading (kg/m2)
3.1
 
400
829
Aspect ratio
1.7
 
11.5
25.6
Rotors
Rotor number (qt)
1
 
4
8
Weights
Empty weight (kg)
8
 
36,850
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
63,600
575,000
Loaded weight (kg)
5
 
47,850
242,500
Capacity
Crew (per.)
1
 
11
112
Speeds
Max. Speed (km/h)
25
 
558
28,165
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
9,600
60,000
4 powerplants
Performance
Service ceiling (m)
0.6
 
11,200
161,544
Takeoff roll (m)
20
 
960
3,200
Landing roll (m)
20
 
920
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
276
36,000
Time to altitude (min)
0.6
 
18.2
105
to 5000 m
Propellers
Prop diameter (m)
1.8
 
5.1
5.8
Prop blade number (qt)
1
 
4
8
Stat
Number built (qt)
0
 
847
43,000
Introduction 1949
First flight 19.05.1947
Stop production 1960

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