Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      50 kg/m2
      76 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
      922 kg
      1384 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1360 kg
      2040 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
      96 km/h
      1500 km/h
    • Max. Speed
      214 km/h
      322 km/h
    • Сruise Speed
      194 km/h
      292 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
      360 hp
      541 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5680 m
      8520 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
      308 m/min
      462 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      16 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Polikarpov DI-1

TypeAircraft
Company

Polikarpov Design Bureau

Scheme

Biplane

Geometry
Length (m)
1.9
 
9.8
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
27.2
925
Wingspan (Beam) (m)
0.1
 
12
95
Wing loading (kg/m2)
3.1
 
63
829
Weights
Empty weight (kg)
8
 
1,153
276,800
Loaded weight (kg)
5
 
1,700
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
268
28,165
Сruise Speed (km/h)
52
 
243
3,087
Power
Total Power (hp)
0.4
 
450.4
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
7,100
161,544
Range (Ferry range) (km)
4
 
800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
385
36,000
Time to altitude (min)
0.6
 
13
105
to 5000 m
Combat
Guns (qt)
1
 
2
18
7.62 mm (0.30 in) machine guns
Stat
Number built (qt)
0
 
1
43,000
Introduction 1926
First flight 12.01.1926

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