Search filter

    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      7 m
      11 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
      307 kg
      461 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      460 kg
      690 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
      96 km/h
      1500 km/h
    • Max. Speed
      120 km/h
      180 km/h
    • Сruise Speed
      94 km/h
      142 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
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 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
      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
      201 m/min
      303 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
      2 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
      43000 qt
    • Price
      41 USD
      750000000 USD

Fokker D.II

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.4
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
18
925
Wingspan (Beam) (m)
0.1
 
8.8
95
Weights
Empty weight (kg)
8
 
384
276,800
Loaded weight (kg)
5
 
575
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
150
28,165
Сruise Speed (km/h)
52
 
118
3,087
Power
Total Power (hp)
0.4
 
100
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Endurance (h)
0.0
 
1.3
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
252
36,000
Combat
Guns (qt)
1
 
1
18
fixed, forward-firing 7.92 mm (.312 in) lMG 08 machine gun
Stat
Introduction 1916

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