Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      52 m2
      80 m2
    • Wingspan (Beam)
      16 m
      26 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
      3720 kg
      5580 kg
    • Max. takeoff weight (Gross weight)
      6120 kg
      9180 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
      333 km/h
      501 km/h
    • Сruise Speed
      268 km/h
      402 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
      1480 hp
      2220 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6840 m
      10260 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1240 km
      1860 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
      324 m/min
      486 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      16 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      12 qt
      20 qt
    • Price
      41 USD
      750000000 USD

Fokker T.V

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
66.2
925
Wingspan (Beam) (m)
0.1
 
21
95
Weights
Empty weight (kg)
8
 
4,650
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,650
575,000
Capacity
Crew (per.)
1
 
5
112
Pilot, co-pilot, bombardier, radioman/gunner, gunner
Speeds
Max. Speed (km/h)
25
 
417
28,165
Сruise Speed (km/h)
52
 
335
3,087
Power
Total Power (hp)
0.4
 
1,850
60,000
2 powerplants 925 hp each at 2 896 m
Performance
Service ceiling (m)
0.6
 
8,550
161,544
Range (Ferry range) (km)
4
 
1,550
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
405
36,000
Time to altitude (min)
0.6
 
13.1
105
to 5000 m
Combat
Guns (qt)
1
 
6
18
1 × 20 mm Solothurn S-18/100 cannon in nose cupola; 5 × 7.9 mm (.31 in) machine-guns on dorsal, ventral, and lateral positions, and tail cupola
Bombs weight (kg)
2
 
1,000
39,000
Stat
Number built (qt)
0
 
16
43,000
Introduction 1937
First flight 16.10.1937
Stop production 1940

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