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    • Year
      1906
      2018
    • Length
      4 m
      7 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      23 m2
    • Wingspan (Beam)
      5 m
      9 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      3
      5
    • 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
      324 kg
      488 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      468 kg
      704 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
      148 km/h
      222 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      121 km/h
      183 km/h
    • Stall Speed
      57 km/h
      87 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
      88 hp
      132 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4876 m
      7314 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      240 km
      360 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      2 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
      273 m/min
      411 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
      256 qt
      384 qt
    • Price
      41 USD
      750000000 USD

Fokker Dr.I

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Triplane

Geometry
Length (m)
1.9
 
5.8
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
18.7
925
Wingspan (Beam) (m)
0.1
 
7.2
95
Aspect ratio
1.7
 
4.0
25.6
Weights
Empty weight (kg)
8
 
406
276,800
Loaded weight (kg)
5
 
586
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
185
1,500
at sea level
Сruise Speed (km/h)
52
 
152
3,087
Stall Speed (km/h)
40
 
72
257.7
Power
Total Power (hp)
0.4
 
110
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,095
161,544
Range (Ferry range) (km)
4
 
300
40,700
Endurance (h)
0.0
 
1.5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
342
36,000
Combat
Guns (qt)
1
 
2
18
7.92 mm (.312 in) "Spandau" lMG 08 machine guns.
Stat
Number built (qt)
0
 
320
43,000
Introduction 1917
First flight 05.07.1917

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