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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      54 m2
    • Wingspan (Beam)
      11 m
      17 m
    • Wing loading
      39 kg/m2
      60 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
      1152 kg
      1730 kg
    • Max. takeoff weight (Gross weight)
      1685 kg
      2529 kg
    • Loaded weight
      5 kg
      242500 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
      161 km/h
      243 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      140 km/h
      212 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
      320 hp
      480 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3840 m
      5760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      7 h
    • Takeoff roll
      200 m
      300 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      176 m/min
      264 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 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
      1597 qt
      2397 qt
    • Price
      41 USD
      750000000 USD

Polikarpov R-1

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.2
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
45
925
both wings
Wingspan (Beam) (m)
0.1
 
14.0
95
Wing loading (kg/m2)
3.1
 
49.2
829
Weights
Empty weight (kg)
8
 
1,441
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,106.9
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
202
1,500
Сruise Speed (km/h)
52
 
176
3,087
Power
Total Power (hp)
0.4
 
400
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,800
161,544
Endurance (h)
0.0
 
5.3
150
Takeoff roll (m)
20
 
250
3,200
Dynamic Performance
Rate of climb (m/min)
1.9
 
220
36,000
Combat
Guns (qt)
1
 
3
18
1 × 7,62 mm machine gun; 2 х 7,62 mm Lewis guns
Stat
Number built (qt)
0
 
1,997
43,000
Introduction 1918
First flight 01.03.1918
Stop production 1931

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