Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      22 m2
      34 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      52 kg/m2
      80 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
      1120 kg
      1680 kg
    • Max. takeoff weight (Gross weight)
      1476 kg
      2216 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 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
      222 km/h
      334 km/h
    • Max. Speed
      222 km/h
      334 km/h
    • Сruise Speed
      196 km/h
      296 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
      584 hp
      877 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5760 m
      8640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      468 km
      702 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
      400 m/min
      600 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      16 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      3 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
      311 qt
      467 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-3

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
27.9
925
Wingspan (Beam) (m)
0.1
 
11
95
Wing loading (kg/m2)
3.1
 
66
829
Weights
Empty weight (kg)
8
 
1,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,846
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
278
1,500
Max. Speed (km/h)
25
 
278
28,165
Сruise Speed (km/h)
52
 
246
3,087
Power
Total Power (hp)
0.4
 
730.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,200
161,544
Range (Ferry range) (km)
4
 
585
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
500
36,000
Time to altitude (min)
0.6
 
12.6
105
to 5000 m
Combat
Guns (qt)
1
 
2
18
7.62 mm (0.3 in) PV-1 machine guns
Stat
Number built (qt)
0
 
389
43,000
Introduction 1928
First flight 21.02.1928
Stop production 1935

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