Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      40 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      32 kg/m2
      50 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
      1358 kg
      2038 kg
    • Max. takeoff weight (Gross weight)
      2380 kg
      3572 kg
    • Loaded weight
      1816 kg
      2726 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      458 kg
      688 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      121 km/h
      183 km/h
    • Сruise Speed
      88 km/h
      132 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
      99 hp
      150 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2400 m
      3600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      504 km
      756 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
      133 m/min
      201 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
      1 qt
      2 qt
    • Bombs
      4 qt
      8 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      16000 qt
      24000 qt
    • Price
      41 USD
      750000000 USD

Polikarpov Po-2

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.2
88.7
Height (m)
0.6
 
3.1
50.1
Wings
Wing area (m2)
1.1
 
33.2
925
Wingspan (Beam) (m)
0.1
 
11.4
95
Wing loading (kg/m2)
3.1
 
41
829
Weights
Empty weight (kg)
8
 
770
276,800
8
 
1,698
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,350
575,000
154
 
2,976
575,000
Loaded weight (kg)
5
 
2,271
242,500
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
573
90,700
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
152
28,165
Сruise Speed (km/h)
52
 
110
3,087
Power
Total Power (hp)
0.4
 
124.7
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,000
161,544
Range (Ferry range) (km)
4
 
630
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
166.8
36,000
Combat
Guns (qt)
1
 
1
18
7.62×54mmR (0.30 in) ShKAS machine gun
Bombs (qt)
1
 
6
250
50 kg (110 lb) bombs
Stat
Number built (qt)
0
 
20,000
43,000
Introduction 1944
First flight 24.06.1927

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