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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      16 m2
      25 m2
    • Wingspan (Beam)
      7 m
      11 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
      536 kg
      804 kg
    • Max. takeoff weight (Gross weight)
      724 kg
      1088 kg
    • Loaded weight
      724 kg
      1088 kg
    • Crew
      1 per.
      2 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
      151 km/h
      227 km/h
    • Сruise Speed
      148 km/h
      224 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
      128 hp
      192 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      2 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
      188 m/min
      283 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      3 min
      6 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
      2640 qt
      3960 qt
    • Price
      41 USD
      750000000 USD

Fokker D.VII

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.0
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
20.5
925
Wingspan (Beam) (m)
0.1
 
8.9
95
Weights
Empty weight (kg)
8
 
670
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
906
575,000
Loaded weight (kg)
5
 
906
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
189
28,165
Сruise Speed (km/h)
52
 
186
3,087
Power
Total Power (hp)
0.4
 
160
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Endurance (h)
0.0
 
1.5
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
235.2
36,000
Time to altitude (min)
0.6
 
28.1
105
to 5000 m
0.6
 
22.8
105
to 4000 m
0.6
 
13.8
105
to 3000 m
0.6
 
8.3
105
to 2000 m
0.6
 
4.3
105
to 1000 m
Combat
Guns (qt)
1
 
2
18
7.92 mm (.312 in) LMG 08/15 "Spandau" machine guns
Stat
Number built (qt)
0
 
3,300
43,000
Introduction 1918
First flight 1918

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