Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      8 m
      12 m
    • Wing loading
      172 kg/m2
      260 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
      2328 kg
      3492 kg
    • Max. takeoff weight (Gross weight)
      2856 kg
      4284 kg
    • Loaded weight
      2856 kg
      4284 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
      432 km/h
      648 km/h
    • Max. Speed
      524 km/h
      786 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
      1360 hp
      2040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9200 m
      13800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      784 km
      1176 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
      668 m/min
      1002 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      8 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Polikarpov ITP

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
9.2
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
16.5
925
Wingspan (Beam) (m)
0.1
 
10
95
Wing loading (kg/m2)
3.1
 
216
829
Weights
Empty weight (kg)
8
 
2,910
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,570
575,000
Loaded weight (kg)
5
 
3,570
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
540
1,500
Max. Speed (km/h)
25
 
655
28,165
Power
Total Power (hp)
0.4
 
1,700
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,500
161,544
Range (Ferry range) (km)
4
 
980
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
835
36,000
Time to altitude (min)
0.6
 
6
105
to 5000 m
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
3
18
20 mm ShVAK cannons, 200 rpg
Rockets (qt)
1
 
8
76
unguided RS-82
Stat
Number built (qt)
0
 
2
43,000
Introduction 1942
First flight 23.02.1942

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