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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      144 m2
    • Wingspan (Beam)
      22 m
      35 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
      3616 kg
      5424 kg
    • Max. takeoff weight (Gross weight)
      5448 kg
      8172 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 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
      142 km/h
      214 km/h
    • Сruise Speed
      142 km/h
      214 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
      1088 hp
      1632 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3864 m
      5796 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      152 m/min
      230 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
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      174 qt
      262 qt
    • Price
      41 USD
      750000000 USD

Tupolev G-1

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
18
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
120
925
Wingspan (Beam) (m)
0.1
 
28.7
95
Weights
Empty weight (kg)
8
 
4,520
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,810
575,000
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
178
28,165
Сruise Speed (km/h)
52
 
178
3,087
Power
Total Power (hp)
0.4
 
1,360
60,000
2 powerplants 680 hp each
Performance
Service ceiling (m)
0.6
 
4,830
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
191.1
36,000
Combat
Guns (qt)
1
 
6
18
6 × DA machine guns
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
218
43,000
Introduction 1929
First flight 26.11.1925
Stop production 1948

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