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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      78 m2
      118 m2
    • Wingspan (Beam)
      20 m
      32 m
    • Wing loading
      58 kg/m2
      89 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
      3732 kg
      5598 kg
    • Max. takeoff weight (Gross weight)
      5760 kg
      8640 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      208 km/h
      312 km/h
    • Сruise Speed
      172 km/h
      258 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
      1200 hp
      1800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4720 m
      7080 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1248 km
      1872 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
      2 qt
    • Bombs weight
      640 kg
      960 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      26 qt
      40 qt
    • Price
      41 USD
      750000000 USD

Fokker T.IV

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
17.6
88.7
Height (m)
0.6
 
6
50.1
Wings
Wing area (m2)
1.1
 
97.8
925
Wingspan (Beam) (m)
0.1
 
26.2
95
Wing loading (kg/m2)
3.1
 
73.6
829
Weights
Empty weight (kg)
8
 
4,665
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,200
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
260
28,165
Сruise Speed (km/h)
52
 
215
3,087
Power
Total Power (hp)
0.4
 
1,500
60,000
2 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
5,900
161,544
Range (Ferry range) (km)
4
 
1,560
40,700
Combat
Guns (qt)
1
 
3
18
7.9 mm (.31 in) Browning machine gun each in nose and dorsal turrets and ventral position
Torpedoes (qt)
1
 
1
4
externally or
Bombs weight (kg)
2
 
800
39,000
bombs internally
Stat
Number built (qt)
0
 
33
43,000
Introduction 1927
First flight 1927
Stop production 1942

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