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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      44 m2
      67 m2
    • Wingspan (Beam)
      15 m
      24 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
      3120 kg
      4680 kg
    • Max. takeoff weight (Gross weight)
      4240 kg
      6360 kg
    • Loaded weight
      4240 kg
      6360 kg
    • Crew
      2 per.
      4 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
      236 km/h
      356 km/h
    • Max. Speed
      281 km/h
      423 km/h
    • Сruise Speed
      256 km/h
      386 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
      857 l
      1287 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
      1630 hp
      2446 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7336 m
      11004 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
      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
      420 m/min
      632 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
      2 qt
      4 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 DIP

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.2
88.7
Height (m)
0.6
 
5.5
50.1
Wings
Wing area (m2)
1.1
 
55.1
925
Wingspan (Beam) (m)
0.1
 
19.2
95
Weights
Empty weight (kg)
8
 
3,900
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,300
575,000
Loaded weight (kg)
5
 
5,300
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
296
1,500
Max. Speed (km/h)
25
 
352
28,165
Сruise Speed (km/h)
52
 
321
3,087
Fuel
Fuel Capacity (l)
23
 
1,072
320,000
Power
Total Power (hp)
0.4
 
2,038
60,000
2 powerplants 1019 hp each
Performance
Service ceiling (m)
0.6
 
9,170
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
526
36,000
Combat
Guns (qt)
1
 
3
18
1 moveable machine gun; 2 recoilless cannon
Stat
Number built (qt)
0
 
1
43,000
Introduction 1935
First flight 01.02.1935

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