Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      27 m2
      42 m2
    • Wingspan (Beam)
      12 m
      19 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
      4640 kg
      6960 kg
    • Max. takeoff weight (Gross weight)
      7174 kg
      10762 kg
    • Loaded weight
      6272 kg
      9408 kg
    • Crew
      1 per.
      3 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
      411 km/h
      617 km/h
    • Max. Speed
      444 km/h
      666 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
      2240 hp
      3360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8200 m
      12300 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1376 km
      2064 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
      444 m/min
      668 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      8 qt
      12 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Polikarpov TIS

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.7
88.7
Height (m)
0.6
 
4.4
50.1
Wings
Wing area (m2)
1.1
 
34.8
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Weights
Empty weight (kg)
8
 
5,800
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,968
575,000
Loaded weight (kg)
5
 
7,840
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
514
1,500
Max. Speed (km/h)
25
 
555
28,165
Power
Total Power (hp)
0.4
 
2,800
60,000
2 powerplants 1400 hp each
Performance
Service ceiling (m)
0.6
 
10,250
161,544
Range (Ferry range) (km)
4
 
1,720
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
556
36,000
Time to altitude (min)
0.6
 
7.3
105
to 5000 m
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
10
18
2 × 20 mm ShVAK cannon (wing roots); 2 × 12.7 mm UBK machine guns (wing roots); 4 × 7.62 mm ShKAS machine guns (nose); 2 × 7.62 mm ShKAS machine guns (flexibly mounted)
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1941
First flight 01.09.1941

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