Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      49 m2
    • Wingspan (Beam)
      13 m
      20 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
      3210 kg
      4816 kg
    • Max. takeoff weight (Gross weight)
      5162 kg
      7744 kg
    • Loaded weight
      5162 kg
      7744 kg
    • Crew
      2 per.
      4 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
      360 km/h
      540 km/h
    • Max. Speed
      424 km/h
      636 km/h
    • Сruise Speed
      333 km/h
      501 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
      1536 hp
      2304 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      476 m/min
      714 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
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Polikarpov VIT-1

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
12.7
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
40.4
925
Wingspan (Beam) (m)
0.1
 
16.5
95
Weights
Empty weight (kg)
8
 
4,013
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,453
575,000
Loaded weight (kg)
5
 
6,453
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
450
1,500
Max. Speed (km/h)
25
 
530
28,165
at 3000 m
Сruise Speed (km/h)
52
 
417
3,087
Power
Total Power (hp)
0.4
 
1,920
60,000
2 powerplants 960 hp each
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
595
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
4
18
2 x 37 mm Sh-37 cannon; 1x 20 mm ShVAK cannon; 1x 7.62 mm ShKAS machine gun
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
1
43,000
Introduction 1937
First flight 1937

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