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    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      48 m2
    • Wingspan (Beam)
      10 m
      16 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
      1372 kg
      2058 kg
    • Max. takeoff weight (Gross weight)
      2040 kg
      3060 kg
    • Loaded weight
      2036 kg
      3054 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
      224 km/h
      336 km/h
    • Сruise Speed
      188 km/h
      282 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
      620 hp
      930 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5120 m
      7680 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      584 km
      876 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
      230 m/min
      346 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
      3 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
      11 qt
      17 qt
    • Price
      41 USD
      750000000 USD

Fokker C.XI

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Biplane

Geometry
Length (m)
1.9
 
10.4
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
40
925
Wingspan (Beam) (m)
0.1
 
13
95
Weights
Empty weight (kg)
8
 
1,715
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,550
575,000
Loaded weight (kg)
5
 
2,545
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
280
28,165
Сruise Speed (km/h)
52
 
235
3,087
Power
Total Power (hp)
0.4
 
775
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,400
161,544
Range (Ferry range) (km)
4
 
730
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
288
36,000
Combat
Guns (qt)
1
 
2
18
1 × fixed, forward-firing 7.9 mm (.31 in) FN-Browning machine gun in forward fuselage; 1 × trainable, rearward-firing 7.9 mm (.31 in) FN-Browning machine gun in observer's cockpit
Stat
Number built (qt)
0
 
14
43,000
Introduction 1935
First flight 1935

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