Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      52 kg/m2
      78 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
      132 kg
      198 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 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
      228 km/h
      342 km/h
    • Max. Speed
      296 km/h
      444 km/h
    • Сruise Speed
      52 km/h
      3087 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
      378 hp
      568 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5800 m
      8700 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      600 km
      900 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
      364 m/min
      548 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      2 m
      4 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      80 kg
      120 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2650 qt
      3976 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-15

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.1
88.7
Height (m)
0.6
 
2.2
50.1
Wings
Wing area (m2)
1.1
 
21.9
925
both wings
Wingspan (Beam) (m)
0.1
 
9.8
95
Wing loading (kg/m2)
3.1
 
65
829
Weights
Empty weight (kg)
8
 
165
276,800
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
285
1,500
Max. Speed (km/h)
25
 
370
28,165
Power
Total Power (hp)
0.4
 
473.2
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,250
161,544
Range (Ferry range) (km)
4
 
750
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
456
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
2.9
5.8
Combat
Guns (qt)
1
 
4
18
fixed forward-firing 7.62×54mmR PV-1 machine guns
Bombs weight (kg)
2
 
100
39,000
Stat
Number built (qt)
0
 
3,313
43,000
Introduction 1933
First flight 01.10.1933

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