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    • Year
      1906
      2018
    • Length
      17 m
      27 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      115 m2
      174 m2
    • Wingspan (Beam)
      29 m
      44 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
      10400 kg
      15600 kg
    • Max. takeoff weight (Gross weight)
      16800 kg
      25200 kg
    • Loaded weight
      15200 kg
      22800 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
      292 km/h
      438 km/h
    • Max. Speed
      284 km/h
      426 km/h
    • Сruise Speed
      256 km/h
      384 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
      3040 hp
      4560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5199 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1456 km
      2184 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      15 h
      23 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
      184 m/min
      276 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      3200 kg
      4800 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Tupolev MTB-2

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
22.4
88.7
Height (m)
0.6
 
7.9
50.1
Wings
Wing area (m2)
1.1
 
144.7
925
Wingspan (Beam) (m)
0.1
 
36.5
95
Weights
Empty weight (kg)
8
 
13,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
21,000
575,000
Loaded weight (kg)
5
 
19,000
242,500
Capacity
Crew (per.)
1
 
7
112
or 8
Speeds
Ground Speed (km/h)
96.6
 
365
1,500
Max. Speed (km/h)
25
 
355
28,165
Сruise Speed (km/h)
52
 
320
3,087
Power
Total Power (hp)
0.4
 
3,800
60,000
4 powerplants 950 hp each
Performance
Service ceiling (m)
0.6
 
6,499.9
161,544
Range (Ferry range) (km)
4
 
1,820
40,700
Endurance (h)
0.0
 
19
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
230
36,000
Combat
Guns (qt)
1
 
6
18
2 20mm ShVAK cannon, 4 7.62mm ShKAS machine guns
Bombs weight (kg)
2
 
4,000
39,000
2000kg-4000kg bombs
Stat
Number built (qt)
0
 
2
43,000
Introduction 1937
First flight 19.04.1937

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