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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      61 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      51 kg/m2
      78 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
      1575 kg
      2363 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2597 kg
      3897 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
      186 km/h
      280 km/h
    • Max. Speed
      182 km/h
      274 km/h
    • Сruise Speed
      156 km/h
      236 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
      543 hp
      816 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5120 m
      7680 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      1 m/min
      3 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      200 kg
      300 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      5600 qt
      8400 qt
    • Price
      41 USD
      750000000 USD

Polikarpov R-5

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.6
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
50.2
925
Wingspan (Beam) (m)
0.1
 
15.5
95
Wing loading (kg/m2)
3.1
 
64.7
829
Weights
Empty weight (kg)
8
 
1,969
276,800
Loaded weight (kg)
5
 
3,247
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
233
1,500
Max. Speed (km/h)
25
 
228
28,165
Сruise Speed (km/h)
52
 
196
3,087
Power
Total Power (hp)
0.4
 
679.6
60,000
Performance
Service ceiling (m)
0.6
 
6,400
161,544
Range (Ferry range) (km)
4
 
800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
2.1
36,000
to 1000 m
Combat
Guns (qt)
1
 
2
18
1 fixed forward firing PV-1 machine gun and 1 DA machine gun in rear cockpit
Bombs weight (kg)
2
 
250
39,000
bombs on bomb racks
Stat
Number built (qt)
0
 
7,000
43,000
Introduction 1935
First flight 1928
Stop production 1944

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