Search filter

    • Year
      1906
      2018
    • Length
      27 m
      42 m
    • Height
      8 m
      13 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      132 m2
      198 m2
    • Wingspan (Beam)
      26 m
      40 m
    • Wing loading
      368 kg/m2
      552 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
      29760 kg
      44640 kg
    • Max. takeoff weight (Gross weight)
      63200 kg
      94800 kg
    • Loaded weight
      60800 kg
      91200 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
      96 km/h
      1500 km/h
    • Max. Speed
      840 km/h
      1260 km/h
    • Сruise Speed
      624 km/h
      936 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10240 m
      15360 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5760 km
      8640 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2440 km
      3660 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
      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
      5 qt
      9 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
      1207 qt
      1811 qt
    • Price
      41 USD
      750000000 USD

Tupolev 88

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
34.8
88.7
Height (m)
0.6
 
10.4
50.1
Wings
Wing area (m2)
1.1
 
165
925
Wingspan (Beam) (m)
0.1
 
33
95
Wing loading (kg/m2)
3.1
 
460
829
Weights
Empty weight (kg)
8
 
37,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
79,000
575,000
Loaded weight (kg)
5
 
76,000
242,500
Capacity
Crew (per.)
1
 
7
112
or 6
Speeds
Max. Speed (km/h)
25
 
1,050
28,165
Сruise Speed (km/h)
52
 
780
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.2
2.1
Performance
Service ceiling (m)
0.6
 
12,800
161,544
Range (Ferry range) (km)
4
 
7,200
40,700
Сombat radius (km)
277
 
3,050
7,210
Combat
Guns (qt)
1
 
7
18
6–7 × 23 mm Afanasev Makarov AM-23 cannons
Stat
Number built (qt)
0
 
1,509
43,000
Introduction 1958
First flight 27.04.1952
Stop production 1993

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