Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      9 m
      15 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
      3012 kg
      4518 kg
    • Max. takeoff weight (Gross weight)
      4280 kg
      6420 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
      584 km/h
      876 km/h
    • Сruise Speed
      471 km/h
      707 km/h
    • Stall Speed
      113 km/h
      171 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
      0 hp
      60000 hp
    • Thrust
      12 kN
      19 kN
    • Service ceiling
      9200 m
      13800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      760 km
      1140 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
      782 m/min
      1174 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
      16 qt
      26 qt
    • Price
      41 USD
      750000000 USD

Fokker S-14 Machtrainer

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.3
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
31.8
925
Wingspan (Beam) (m)
0.1
 
12
95
Weights
Empty weight (kg)
8
 
3,765
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,350
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
730
28,165
Сruise Speed (km/h)
52
 
589
3,087
Stall Speed (km/h)
40
 
142
257.7
Power
Thrust (kN)
1.5
 
15.4
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,500
161,544
Range (Ferry range) (km)
4
 
950
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
978
36,000
Stat
Number built (qt)
0
 
21
43,000
Introduction 1951
First flight 19.05.1951
Stop production 1967

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