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
      11 m2
      18 m2
    • Wingspan (Beam)
      7 m
      11 m
    • Wing loading
      107 kg/m2
      161 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
      1192 kg
      1788 kg
    • Max. takeoff weight (Gross weight)
      1676 kg
      2514 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
      330 km/h
      496 km/h
    • Max. Speed
      420 km/h
      630 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
      879 hp
      1320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7760 m
      11640 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      560 km
      840 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
      705 m/min
      1059 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      7 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
      4 qt
      8 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      400 kg
      600 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      6915 qt
      10373 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-16

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
6.1
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
14.5
925
Wingspan (Beam) (m)
0.1
 
9
95
Wing loading (kg/m2)
3.1
 
134
829
Weights
Empty weight (kg)
8
 
1,490
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,095
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
413
1,500
Max. Speed (km/h)
25
 
525
28,165
at 3000 m
Power
Total Power (hp)
0.4
 
1,099.2
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
9,700
161,544
Range (Ferry range) (km)
4
 
700
40,700
with drop tanks
Dynamic Performance
Rate of climb (m/min)
1.9
 
882
36,000
Time to altitude (min)
0.6
 
5.8
105
to 5000 m
Combat
Guns (qt)
1
 
4
18
2 × fixed forward-firing 7.62 mm (0.30 in) ShKAS machine guns in upper cowling; 2 × fixed forward-firing 20 mm (0.79 in) ShVAK cannons in the wings
Rockets (qt)
1
 
6
76
unguided RS-82 rockets or
Bombs weight (kg)
2
 
500
39,000
Stat
Number built (qt)
0
 
8,644
43,000
Introduction 1939
First flight 30.12.1933
Stop production 1950

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