Search filter

    • Year
      1906
      2018
    • Length
      28 m
      43 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      74 m2
      113 m2
    • Wingspan (Beam)
      22 m
      34 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
      19500 kg
      29250 kg
    • Max. takeoff weight (Gross weight)
      34472 kg
      51708 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
      175 per.
      263 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      684 km/h
      1026 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
      10692 l
      16038 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
      98 kN
      148 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1960 km
      2940 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
      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
      226 qt
      340 qt
    • Price
      41 USD
      750000000 USD

Fokker 100

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
35.5
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wing area (m2)
1.1
 
93.5
925
Wingspan (Beam) (m)
0.1
 
28.1
95
Weights
Empty weight (kg)
8
 
24,375
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
43,090
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
219
400
122 (1-class, maximum); 107 (1-class, typical); 97 (2-class, typical)
Speeds
Сruise Speed (km/h)
52
 
855
3,087
Fuel
Fuel Capacity (l)
23
 
13,365
320,000
Power
Thrust (kN)
1.5
 
123.2
1,914
2 powerplants 61,6 kN each
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
2,450
40,700
fully loaded
Stat
Number built (qt)
0
 
283
43,000
Introduction 1986
First flight 30.11.1986

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