Search filter

    • Year
      1906
      2018
    • Length
      27 m
      42 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
      28209 kg
      42315 kg
    • Max. takeoff weight (Gross weight)
      56245 kg
      84369 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      18524 kg
      27788 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      456 km/h
      684 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
      23 l
      320000 l
    • Fuel External
      142 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
      14416 hp
      21624 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5608 m
      8413 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1976 km
      2965 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Lockheed L-100 Hercules

TypeAircraft
Company

Lockheed Corporation

Geometry
Length (m)
1.9
 
34.4
88.7
Height (m)
0.6
 
11.7
50.1
Wings
Wing area (m2)
1.1
 
162.1
925
Wingspan (Beam) (m)
0.1
 
40.4
95
Weights
Empty weight (kg)
8
 
35,262.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
70,306.8
575,000
Capacity
Payload (kg)
23
 
23,155.9
122,470
Speeds
Max. Speed (km/h)
25
 
570
28,165
at 6100
Power
Total Power (hp)
0.4
 
18,020
60,000
4 powerplants 4505 hp each
Performance
Service ceiling (m)
0.6
 
7,010.4
161,544
Range (Ferry range) (km)
4
 
2,470.6
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
557.8
36,000
Stat
Introduction 30.09.1965
First flight 20.04.1964

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