Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      65 m2
      99 m2
    • Wingspan (Beam)
      18 m
      28 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
      2680 kg
      4020 kg
    • Max. takeoff weight (Gross weight)
      4640 kg
      6960 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
      12 per.
      18 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      112 km/h
      168 km/h
    • Сruise Speed
      93 km/h
      141 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
      768 hp
      1152 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      560 km
      840 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
      1 m/min
      36000 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
      18 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
      8 qt
      14 qt
    • Price
      41 USD
      750000000 USD

Fokker F.VIII

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
16.8
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
82
925
Wingspan (Beam) (m)
0.1
 
23
95
Weights
Empty weight (kg)
8
 
3,350
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,800
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
15
400
Speeds
Max. Speed (km/h)
25
 
140
28,165
Сruise Speed (km/h)
52
 
117
3,087
Power
Total Power (hp)
0.4
 
960
60,000
2 powerplants 480 hp each
Performance
Service ceiling (m)
0.6
 
5,500
161,544
Range (Ferry range) (km)
4
 
700
40,700
Stat
Number built (qt)
0
 
11
43,000
Introduction 1927
First flight 12.03.1927

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