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    • Year
      1906
      2018
    • Length
      36 m
      56 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      248 m2
      372 m2
    • Wingspan (Beam)
      40 m
      61 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
      72000 kg
      108000 kg
    • Max. takeoff weight (Gross weight)
      150400 kg
      225600 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      520 km/h
      780 km/h
    • Max. Speed
      736 km/h
      1104 km/h
    • Сruise Speed
      600 km/h
      900 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
      70960 l
      106440 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
      48000 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10960 m
      16440 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      12000 km
      18000 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      5200 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
      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
      400 qt
      600 qt
    • Price
      41 USD
      750000000 USD

Tupolev 95

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
46.2
88.7
Height (m)
0.6
 
12.1
50.1
Wings
Wing area (m2)
1.1
 
310
925
Wingspan (Beam) (m)
0.1
 
50.1
95
Weights
Empty weight (kg)
8
 
90,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
188,000
575,000
Capacity
Crew (per.)
1
 
7
112
Speeds
Ground Speed (km/h)
96.6
 
650
1,500
Max. Speed (km/h)
25
 
920
28,165
Сruise Speed (km/h)
52
 
750
3,087
Fuel
Fuel Capacity (l)
23
 
88,700
320,000
Power
Total Power (hp)
0.4
 
60,000
60,000
4 powerplants 15000 hp each
Performance
Service ceiling (m)
0.6
 
13,700
161,544
Range (Ferry range) (km)
4
 
15,000
40,700
Сombat radius (km)
277
 
6,500
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
600
36,000
Combat
Guns (qt)
1
 
2
18
1 or 2 × 23 mm AM-23 autocannon in tail turret
Stat
Number built (qt)
0
 
500
43,000
Introduction 1979
First flight 12.11.1952

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