Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      24 m2
    • Wingspan (Beam)
      8 m
      13 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
      889 kg
      1335 kg
    • Max. takeoff weight (Gross weight)
      1208 kg
      1812 kg
    • Loaded weight
      1208 kg
      1812 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
      118 km/h
      178 km/h
    • Max. Speed
      211 km/h
      317 km/h
    • Сruise Speed
      158 km/h
      238 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
      5400 m
      8100 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      520 km
      780 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      3 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
      420 m/min
      632 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
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Polikarpov I-1

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.3
88.7
Wings
Wing area (m2)
1.1
 
20
925
Wingspan (Beam) (m)
0.1
 
10.8
95
Weights
Empty weight (kg)
8
 
1,112
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,510
575,000
Loaded weight (kg)
5
 
1,510
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
148
1,500
Max. Speed (km/h)
25
 
264
28,165
Сruise Speed (km/h)
52
 
198
3,087
Power
Total Power (hp)
0.4
 
400
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,750
161,544
Range (Ferry range) (km)
4
 
650
40,700
Endurance (h)
0.0
 
2.5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
526
36,000
Combat
Guns (qt)
1
 
2
18
synchronised 7.62 mm (0.3 in) PV-1 machine guns.
Stat
Number built (qt)
0
 
2
43,000
Introduction 1923
First flight 15.08.1923

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