Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      8 m
      12 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
      1161 kg
      1743 kg
    • Max. takeoff weight (Gross weight)
      1688 kg
      2532 kg
    • Loaded weight
      1568 kg
      2352 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
      292 km/h
      440 km/h
    • Max. Speed
      355 km/h
      533 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
      640 hp
      961 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8560 m
      12840 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      376 km
      564 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
      720 m/min
      1080 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      6 min
      10 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2749 qt
      4125 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-153

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.2
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
22.1
925
Wingspan (Beam) (m)
0.1
 
10
95
Weights
Empty weight (kg)
8
 
1,452
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,110
575,000
Loaded weight (kg)
5
 
1,960
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
366
1,500
Max. Speed (km/h)
25
 
444
28,165
at 4600 m
Power
Total Power (hp)
0.4
 
800.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,700
161,544
Range (Ferry range) (km)
4
 
470
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
900
36,000
Time to altitude (min)
0.6
 
0.9
105
to 1000 m
0.6
 
8.3
105
to 7000 m
Combat
Guns (qt)
1
 
4
18
7.62×54mmR ShKAS machine guns, 2,600 rounds of ammunition total
Stat
Number built (qt)
0
 
3,437
43,000
Introduction 1938
First flight 1938

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