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    • Year
      1906
      2018
    • Length
      19 m
      30 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      187 m2
      282 m2
    • Wingspan (Beam)
      33 m
      51 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
      8960 kg
      13440 kg
    • Max. takeoff weight (Gross weight)
      15440 kg
      23160 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      196 km/h
      294 km/h
    • Max. Speed
      169 km/h
      255 km/h
    • Сruise Speed
      145 km/h
      219 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
      2256 hp
      3384 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3840 m
      5760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1600 km
      2400 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
      60 m/min
      90 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      23 min
      35 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      6 qt
      10 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1600 kg
      2400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      654 qt
      982 qt
    • Price
      41 USD
      750000000 USD

Tupolev G-2

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
24.4
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wing area (m2)
1.1
 
234.5
925
Wingspan (Beam) (m)
0.1
 
41.8
95
Weights
Empty weight (kg)
8
 
11,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
19,300
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
245
1,500
Max. Speed (km/h)
25
 
212
28,165
at 3000 m
Сruise Speed (km/h)
52
 
182
3,087
Power
Total Power (hp)
0.4
 
2,820
60,000
4 powerplants 705 hp each
Performance
Service ceiling (m)
0.6
 
4,800
161,544
Range (Ferry range) (km)
4
 
2,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
75
36,000
Time to altitude (min)
0.6
 
5
105
to 1000 m
0.6
 
29
105
to 3000 m
Combat
Guns (qt)
1
 
8
18
5–8× 7.62 mm DA machine guns
Bombs weight (kg)
2
 
2,000
39,000
Stat
Number built (qt)
0
 
818
43,000
Introduction 1934
First flight 22.12.1930
Stop production 1939

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