Search filter

    • Year
      1906
      2018
    • Length
      15 m
      23 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      42 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      412 kg/m2
      620 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
      8235 kg
      12354 kg
    • Max. takeoff weight (Gross weight)
      15072 kg
      22610 kg
    • Loaded weight
      14426 kg
      21640 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
      1958 km/h
      2938 km/h
    • Сruise Speed
      772 km/h
      1158 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      87 kN
      131 kN
    • Service ceiling
      12972 m
      19459 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3108 km
      4662 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
      9729 m/min
      14594 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
      3600 kg
      5400 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

North American Aviation F-107 Ultra Sabre

TypeAircraft
Company

North American Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
18.9
88.7
Height (m)
0.6
 
5.9
50.1
Wings
Wing area (m2)
1.1
 
35
925
Wingspan (Beam) (m)
0.1
 
11.2
95
Wing loading (kg/m2)
3.1
 
516
829
Weights
Empty weight (kg)
8
 
10,294.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
18,840.9
575,000
Loaded weight (kg)
5
 
18,033
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
2,448
28,165
Сruise Speed (km/h)
52
 
965
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Thrust (kN)
1.5
 
109
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
16,215.4
161,544
Range (Ferry range) (km)
4
 
3,885
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
12,161.5
36,000
Combat
Bombs weight (kg)
2
 
4,500
39,000
Stat
Number built (qt)
0
 
3
43,000
Introduction 1956
First flight 10.09.1956
Stop production 25.11.1957

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