Search filter

    • Year
      1906
      2018
    • Length
      16 m
      25 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      51 m2
      77 m2
    • Wingspan (Beam)
      17 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
      9743 kg
      14615 kg
    • Max. takeoff weight (Gross weight)
      15966 kg
      23950 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
      35 per.
      53 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      563 km/h
      845 km/h
    • Сruise Speed
      52 km/h
      3087 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
      5056 l
      7584 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
      0 hp
      60000 hp
    • Thrust
      53 kN
      80 kN
    • Service ceiling
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      956 km
      1434 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
      756 m/min
      1134 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Fokker Fokker-VFW 614

TypeAircraft
Company

Fokker Aviatik GmbH

VFW-Fokker

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
20.6
88.7
Height (m)
0.6
 
7.8
50.1
Wings
Wing area (m2)
1.1
 
64
925
Wingspan (Beam) (m)
0.1
 
21.5
95
Weights
Empty weight (kg)
8
 
12,179
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
19,958
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
44
400
40-44 passengers in 4 abreast seating
Speeds
Max. Speed (km/h)
25
 
704
28,165
Fuel
Fuel Capacity (l)
23
 
6,320
320,000
Power
Thrust (kN)
1.5
 
66.4
1,914
2 powerplants 33,2 kN each
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
1,195
40,700
with 40 passengers
Dynamic Performance
Rate of climb (m/min)
1.9
 
945
36,000
Stat
Introduction 1971
First flight 14.07.1971

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