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    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      52 m2
      79 m2
    • Wingspan (Beam)
      12 m
      20 m
    • Wing loading
      246 kg/m2
      370 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
      11871 kg
      17807 kg
    • Max. takeoff weight (Gross weight)
      22892 kg
      34338 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
      885 km/h
      1329 km/h
    • Max. Speed
      1698 km/h
      2548 km/h
    • Сruise Speed
      52 km/h
      3087 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
      10900 l
      16350 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
      121 kN/kg
      183 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      76 kN
      116 kN
    • Service ceiling
      12704 m
      19057 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2960 km
      4440 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1660 km
      2490 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
      1950 m/min
      2927 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
      2 qt
      4 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
      124 qt
      188 qt
    • Price
      41 USD
      750000000 USD

North American Aviation A-5 Vigilante

TypeAircraft
Company

North American Aviation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
23.3
88.7
Height (m)
0.6
 
5.9
50.1
Wings
Wing area (m2)
1.1
 
65.1
925
Wingspan (Beam) (m)
0.1
 
16.2
95
Wing loading (kg/m2)
3.1
 
308.3
829
Weights
Empty weight (kg)
8
 
14,838.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
28,615
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
1,107
1,500
Max. Speed (km/h)
25
 
2,123
28,165
at 12200 m
Fuel
Fuel Capacity (l)
23
 
13,625
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.7
2.1
Afterburning thrust (kN/kg)
29.4
 
152
980
2 powerplants 76 kN each
Thrust (kN)
1.5
 
96
1,914
2 powerplants 48 kN each
Performance
Service ceiling (m)
0.6
 
15,880.1
161,544
Range (Ferry range) (km)
4
 
3,700
40,700
Сombat radius (km)
277
 
2,075
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,438.4
36,000
Combat
Guns (qt)
1
 
3
18
1× Mark 27 nuclear bomb, B28 or B43 freefall nuclear bomb in internal weapons bay; 2× B43, Mark 83, or Mark 84 bombs on two external hardpoints
Stat
Number built (qt)
0
 
156
43,000
Introduction 1958
First flight 31.08.1958
Stop production 20.11.1979

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