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    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      70 m2
      106 m2
    • Wingspan (Beam)
      19 m
      30 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
      5200 kg
      7800 kg
    • Max. takeoff weight (Gross weight)
      8960 kg
      13440 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 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
      352 km/h
      528 km/h
    • Сruise Speed
      318 km/h
      478 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
      2200 hp
      3300 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2176 km
      3264 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1600 kg
      2400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Fokker T.IX

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16.5
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
88.3
925
Wingspan (Beam) (m)
0.1
 
24.7
95
Weights
Empty weight (kg)
8
 
6,500
276,800
equipped
Max. takeoff weight (Gross weight) (kg)
154
 
11,200
575,000
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
440
28,165
Сruise Speed (km/h)
52
 
398
3,087
Power
Total Power (hp)
0.4
 
2,750
60,000
2 powerplants 1375 hp each
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
2,720
40,700
Combat
Guns (qt)
1
 
3
18
intended - one 20mm cannon in nose, twin 12.7mm (0.5in) machine guns in dorsal and ventral positions
Bombs weight (kg)
2
 
2,000
39,000
in internal bomb bay
Stat
Number built (qt)
0
 
1
43,000
Introduction 1939
First flight 11.09.1939

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