Search filter

    • Year
      1906
      2018
    • Length
      19 m
      29 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      137 m2
      207 m2
    • Wingspan (Beam)
      26 m
      40 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
      8240 kg
      12360 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      13200 kg
      19800 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      25 per.
      39 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      252 km/h
      378 km/h
    • Сruise Speed
      224 km/h
      336 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1228 km
      1844 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Fokker F.XXXVI

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
24
88.7
Height (m)
0.6
 
8.3
50.1
Wings
Wing area (m2)
1.1
 
172
925
Wingspan (Beam) (m)
0.1
 
33
95
Weights
Empty weight (kg)
8
 
10,300
276,800
Loaded weight (kg)
5
 
16,500
242,500
Capacity
Crew (per.)
1
 
4
112
Capacity passengers (per.)
1
 
32
400
Speeds
Max. Speed (km/h)
25
 
315
28,165
Сruise Speed (km/h)
52
 
280
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
4 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Range (Ferry range) (km)
4
 
1,536
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1934
First flight 22.06.1934
Stop production 1940

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