Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      23 m2
    • Wingspan (Beam)
      8 m
      14 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
      648 kg
      972 kg
    • Max. takeoff weight (Gross weight)
      880 kg
      1320 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
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      167 km/h
      251 km/h
    • Сruise Speed
      132 km/h
      198 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
      152 hp
      229 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3080 m
      4620 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      502 km
      754 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      3 h
      5 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
      123 m/min
      185 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      4 min
      7 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 S-11

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.2
88.7
Height (m)
0.6
 
2.2
50.1
Wings
Wing area (m2)
1.1
 
18.5
925
Wingspan (Beam) (m)
0.1
 
11
95
Weights
Empty weight (kg)
8
 
810
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,100
575,000
Capacity
Crew (per.)
1
 
2
112
two/three
Speeds
Max. Speed (km/h)
25
 
209
28,165
Сruise Speed (km/h)
52
 
165
3,087
Power
Total Power (hp)
0.4
 
190.4
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,850
161,544
Range (Ferry range) (km)
4
 
628
40,700
Endurance (h)
0.0
 
3.9
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
154
36,000
Time to altitude (min)
0.6
 
5.6
105
to 1000 m
Stat
Introduction 1947
First flight 18.12.1947

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