Search filter

    • Year
      1906
      2018
    • Length
      23 m
      36 m
    • Height
      9 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      129 m2
      195 m2
    • Wingspan (Beam)
      32 m
      49 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
      27520 kg
      41280 kg
    • Max. takeoff weight (Gross weight)
      56240 kg
      84360 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26400 kg
      39600 kg
    • Payload
      16320 kg
      24480 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      473 km/h
      711 km/h
    • Сruise Speed
      432 km/h
      648 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
      8020 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
      14720 hp
      22080 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5661 m
      8493 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3040 km
      4560 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
      446 m/min
      670 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
      1840 qt
      2760 qt
    • Price
      24080000 USD
      36120000 USD

Lockheed C-130 Hercules

TypeAircraft
Company

Lockheed Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
29.8
88.7
Height (m)
0.6
 
11.6
50.1
Wings
Wing area (m2)
1.1
 
162.1
925
Wingspan (Beam) (m)
0.1
 
40.4
95
Weights
Empty weight (kg)
8
 
34,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
70,300
575,000
Capacity
Crew (per.)
1
 
5
112
two pilots, navigator, flight engineer and loadmaster
Useful load (kg)
26.4
 
33,000
90,700
Payload (kg)
23
 
20,400
122,470
Speeds
Max. Speed (km/h)
25
 
592
28,165
at 6060 m
Сruise Speed (km/h)
52
 
540
3,087
Fuel
Fuel External (l)
142.5
 
10,025
10,025
Power
Total Power (hp)
0.4
 
18,400
60,000
4 powerplants 4600 hp each
Performance
Service ceiling (m)
0.6
 
10,060
161,544
empty
0.6
 
7,077
161,544
with 19090 kg payload
Range (Ferry range) (km)
4
 
3,800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
558
36,000
Stat
Number built (qt)
0
 
2,300
43,000
Price (USD)
41.5
 
30.1 million
750.0 million
Introduction 1954
First flight 23.08.1954

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