Search filter

    • Year
      1906
      2018
    • Length
      20 m
      31 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      56 m2
      84 m2
    • Wingspan (Beam)
      23 m
      35 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
      9800 kg
      14700 kg
    • Max. takeoff weight (Gross weight)
      16656 kg
      24984 kg
    • Loaded weight
      14877 kg
      22317 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      46 per.
      70 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      448 km/h
      672 km/h
    • Сruise Speed
      424 km/h
      636 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
      4108 l
      6162 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
      4000 hp
      6000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1644 km
      2466 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
      3 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      4 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
      170 qt
      256 qt
    • Price
      14000000 USD
      21000000 USD

Fokker 50

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
25.3
88.7
Height (m)
0.6
 
8.3
50.1
Wings
Wing area (m2)
1.1
 
70
925
Wingspan (Beam) (m)
0.1
 
29
95
Weights
Empty weight (kg)
8
 
12,250
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,820
575,000
Loaded weight (kg)
5
 
18,597.3
242,500
Capacity
Crew (per.)
1
 
2
112
flight deck crew
Capacity passengers (per.)
1
 
58
400
up to 58 passengers
Speeds
Max. Speed (km/h)
25
 
560
28,165
Сruise Speed (km/h)
52
 
530
3,087
Fuel
Fuel Capacity (l)
23
 
5,135
320,000
Power
Total Power (hp)
0.4
 
5,000
60,000
2 powerplants 2500 hp each
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
2,055
40,700
Propellers
Propellers (qt)
1
 
2
8
Prop blade number (qt)
1
 
6
8
Stat
Number built (qt)
0
 
213
43,000
Price (USD)
41.5
 
17.5 million
750.0 million
Introduction 1985
First flight 28.12.1985

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