Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      29 m2
      45 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      281 kg/m2
      423 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
      7600 kg
      11400 kg
    • Max. takeoff weight (Gross weight)
      12639 kg
      18960 kg
    • Loaded weight
      5 kg
      242500 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
      1112 km/h
      1668 km/h
    • Сruise Speed
      772 km/h
      1160 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
      1 kN/kg
    • Afterburning thrust
      56 kN/kg
      86 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      36 kN
      54 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2568 km
      3852 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
      5462 m/min
      8194 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      3 qt
      5 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2552 kg
      3828 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1835 qt
      2753 qt
    • Price
      557623 USD
      836435 USD

North American Aviation F-100 Super Sabre

TypeAircraft
Company

North American Aviation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
15.2
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
37
925
Wingspan (Beam) (m)
0.1
 
11.8
95
Wing loading (kg/m2)
3.1
 
352
829
Weights
Empty weight (kg)
8
 
9,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,799.5
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,390
28,165
Сruise Speed (km/h)
52
 
966
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Afterburning thrust (kN/kg)
29.4
 
71
980
1 powerplant
Thrust (kN)
1.5
 
45
1,914
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
3,210
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
6,827.5
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.787 in) Pontiac M39A1 revolver cannon
Missiles (qt)
1
 
4
24
AIM-9 Sidewinder or 2 x AGM-12 Bullpup
Bombs weight (kg)
2
 
3,190
39,000
Stat
Number built (qt)
0
 
2,294
43,000
Price (USD)
41.5
 
697,029
750.0 million
Introduction 1953
First flight 25.05.1953
Stop production 1979

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