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    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      44 m2
      67 m2
    • Wingspan (Beam)
      16 m
      26 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
      9645 kg
      14469 kg
    • Max. takeoff weight (Gross weight)
      19065 kg
      28598 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      636 km/h
      954 km/h
    • Max. Speed
      662 km/h
      994 km/h
    • Сruise Speed
      519 km/h
      779 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
      5753 l
      8630 l
    • Fuel External
      1817 l
      2727 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
      66 kN
      100 kN
    • Service ceiling
      9973 m
      14960 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4096 km
      6145 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      682 km
      1024 km
    • Endurance
      5 h
      9 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
      1248 m/min
      1873 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
      1776 kg
      2664 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      150 qt
      226 qt
    • Price
      21600000 USD
      32400000 USD

Lockheed S-3 Viking

TypeAircraft
Company

Lockheed Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
16.3
88.7
Height (m)
0.6
 
6.9
50.1
Wings
Wing area (m2)
1.1
 
55.6
925
Wingspan (Beam) (m)
0.1
 
9
95
Folded
0.1
 
20.9
95
Unfolded
Weights
Empty weight (kg)
8
 
12,056.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
23,831.3
575,000
Capacity
Crew (per.)
1
 
4
112
Pilot, Co-Pilot/COTAC, TACCO, Sensor Operator/TFO
Speeds
Ground Speed (km/h)
96.6
 
795
1,500
at sea level
Max. Speed (km/h)
25
 
828
28,165
at 6100 m
Сruise Speed (km/h)
52
 
649
3,087
Fuel
Fuel Capacity (l)
23
 
7,191.3
320,000
Internal fuel capacity
Fuel External (l)
142.5
 
2,272
10,025
2x 1,136 L tanks
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
82.5
1,914
2 powerplants 41,26 kN each
Performance
Service ceiling (m)
0.6
 
12,466.3
161,544
Range (Ferry range) (km)
4
 
5,120.8
40,700
Сombat radius (km)
277
 
853
7,210
Endurance (h)
0.0
 
7.3
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,560.6
36,000
Combat
Bombs weight (kg)
2
 
2,220
39,000
on four internal and two external hardpoints
Stat
Number built (qt)
0
 
188
43,000
Price (USD)
41.5
 
27.0 million
750.0 million
Introduction 1974
First flight 21.01.1972

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