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    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      46 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      100 kg/m2
      151 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
      2660 kg
      3990 kg
    • Max. takeoff weight (Gross weight)
      4000 kg
      6000 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
      380 km/h
      570 km/h
    • Сruise Speed
      284 km/h
      426 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
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1328 hp
      1992 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8000 m
      12000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1208 km
      1812 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
      648 m/min
      972 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      8 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      7 qt
      11 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      240 kg
      360 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      50 qt
      76 qt
    • Price
      41 USD
      750000000 USD

Fokker G.I

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Twin-boom

Monoplane

Midwing

Geometry
Length (m)
1.9
 
10.9
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
38.3
925
Wingspan (Beam) (m)
0.1
 
17.2
95
Wing loading (kg/m2)
3.1
 
125.3
829
Weights
Empty weight (kg)
8
 
3,325
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,000
575,000
Capacity
Crew (per.)
1
 
2
112
2-3
Speeds
Max. Speed (km/h)
25
 
475
28,165
at 4100
Сruise Speed (km/h)
52
 
355
3,087
Power
Power/mass (hp/kg)
0.0
 
0.3
22.1
Total Power (hp)
0.4
 
1,660
60,000
2 powerplants 830 hp each at 4100
Performance
Service ceiling (m)
0.6
 
10,000
161,544
Range (Ferry range) (km)
4
 
1,510
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
810
36,000
Time to altitude (min)
0.6
 
6.3
105
to 5000
Combat
Guns (qt)
1
 
9
18
8× 7.9 mm (0.31 in) forward-firing FN-Browning machine guns in the nose; 1× 7.9 mm (0.31 in) machine gun in rear turret
Bombs weight (kg)
2
 
300
39,000
Stat
Number built (qt)
0
 
63
43,000
Introduction 1937
First flight 16.03.1937

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