Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      19 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      180 kg/m2
      270 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
      2123 kg
      3185 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2800 kg
      4200 kg
    • Crew
      1 per.
      112 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
      96 km/h
      1500 km/h
    • Max. Speed
      504 km/h
      756 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
      1600 hp
      2400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      668 km
      1002 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
      772 m/min
      1160 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      6 qt
      10 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      400 kg
      600 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-185

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.8
88.7
Height (m)
0.6
 
2.5
50.1
Wings
Wing area (m2)
1.1
 
15.5
925
Wingspan (Beam) (m)
0.1
 
9.8
95
Wing loading (kg/m2)
3.1
 
225
829
Weights
Empty weight (kg)
8
 
2,654
276,800
Loaded weight (kg)
5
 
3,500
242,500
Speeds
Max. Speed (km/h)
25
 
630
28,165
Power
Total Power (hp)
0.4
 
2,000
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
835
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
966
36,000
Combat
Guns (qt)
1
 
3
18
20 mm ShVAK cannons
Rockets (qt)
1
 
8
76
RS-82 rockets or
Bombs weight (kg)
2
 
500
39,000
Stat
Number built (qt)
0
 
4
43,000
Introduction 1940
First flight 11.01.1941

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