Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      64 m2
      96 m2
    • Wingspan (Beam)
      18 m
      28 m
    • Wing loading
      64 kg/m2
      98 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
      3084 kg
      4628 kg
    • Max. takeoff weight (Gross weight)
      5177 kg
      7767 kg
    • Loaded weight
      5177 kg
      7767 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
      208 km/h
      312 km/h
    • Max. Speed
      176 km/h
      264 km/h
    • Сruise Speed
      164 km/h
      246 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1152 hp
      1728 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4840 m
      7260 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1344 km
      2016 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      128 m
      192 m
    • Landing roll
      144 m
      216 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      133 m/min
      201 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
      1 qt
      2 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
      328 qt
      494 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-7

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
15.1
88.7
Wings
Wing area (m2)
1.1
 
80
925
Wingspan (Beam) (m)
0.1
 
23.2
95
Wing loading (kg/m2)
3.1
 
81
829
Weights
Empty weight (kg)
8
 
3,856
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,472
575,000
Loaded weight (kg)
5
 
6,472
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
260
1,500
Max. Speed (km/h)
25
 
220
28,165
Сruise Speed (km/h)
52
 
205
3,087
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
1,440
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
6,050
161,544
Range (Ferry range) (km)
4
 
1,680
40,700
Takeoff roll (m)
20
 
160
3,200
Landing roll (m)
20
 
180
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
167
36,000
Combat
Guns (qt)
1
 
1
18
Stat
Number built (qt)
0
 
411
43,000
Introduction 11.09.1929
First flight 01.05.1930
Stop production 1934

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