Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      7 m
      12 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
      556 kg
      834 kg
    • Max. takeoff weight (Gross weight)
      780 kg
      1170 kg
    • Loaded weight
      780 kg
      1170 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
      148 km/h
      222 km/h
    • Сruise Speed
      121 km/h
      183 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
      98 hp
      148 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3440 m
      5160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      568 km
      852 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
      40 qt
      60 qt
    • Price
      41 USD
      750000000 USD

Fokker S.IX

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.7
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
23
925
Wingspan (Beam) (m)
0.1
 
9.6
95
Weights
Empty weight (kg)
8
 
695
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
975
575,000
Loaded weight (kg)
5
 
975
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and instructor
Speeds
Max. Speed (km/h)
25
 
185
28,165
Сruise Speed (km/h)
52
 
152
3,087
Power
Total Power (hp)
0.4
 
123
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,300
161,544
Range (Ferry range) (km)
4
 
710
40,700
Stat
Number built (qt)
0
 
50
43,000
about 50
Introduction 1937
First flight 01.11.1937

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