Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      8 m
      13 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
      418 kg
      628 kg
    • Max. takeoff weight (Gross weight)
      669 kg
      1005 kg
    • Loaded weight
      668 kg
      1004 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      165 km/h
      249 km/h
    • Max. Speed
      136 km/h
      204 km/h
    • Сruise Speed
      100 km/h
      150 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
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2640 m
      3960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      340 km
      510 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
      50 m/min
      76 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
      18 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
      4 qt
      6 qt
    • Price
      41 USD
      750000000 USD

Tupolev ANT-2

TypeAircraft
Company

Joint Stock Company Tupolev

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
7.6
88.7
Height (m)
0.6
 
2.1
50.1
Wings
Wing area (m2)
1.1
 
17.9
925
Wingspan (Beam) (m)
0.1
 
10.5
95
Weights
Empty weight (kg)
8
 
523
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
837
575,000
Loaded weight (kg)
5
 
836
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Speeds
Ground Speed (km/h)
96.6
 
207
1,500
Max. Speed (km/h)
25
 
170
28,165
Сruise Speed (km/h)
52
 
125
3,087
Power
Total Power (hp)
0.4
 
100
60,000
Performance
Service ceiling (m)
0.6
 
3,300
161,544
Range (Ferry range) (km)
4
 
425
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
63
36,000
Stat
Number built (qt)
0
 
5
43,000
Introduction 1924
First flight 26.05.1924

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