Search filter

    • Year
      1906
      2018
    • Length
      25 m
      39 m
    • Height
      8 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      145 m2
    • Wingspan (Beam)
      24 m
      37 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
      20828 kg
      31244 kg
    • Max. takeoff weight (Gross weight)
      41004 kg
      61508 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 per.
    • Useful load
      12265 kg
      18398 kg
    • Payload
      6350 kg
      9526 kg
    • Capacity passengers
      78 per.
      118 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      312 km/h
      468 km/h
    • Сruise Speed
      480 km/h
      720 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
      16716 l
      25074 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
      12016 hp
      18024 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7802 m
      11705 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3564 km
      5346 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
      480 m/min
      721 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
      136 qt
      204 qt
    • Price
      41 USD
      750000000 USD

Lockheed L-188 Electra

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
31.9
88.7
Height (m)
0.6
 
10
50.1
Wings
Wing area (m2)
1.1
 
120.8
925
Wingspan (Beam) (m)
0.1
 
30.2
95
Weights
Empty weight (kg)
8
 
26,036.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
51,255.9
575,000
Capacity
Crew (per.)
1
 
6
112
Useful load (kg)
26.4
 
15,331.4
90,700
Payload (kg)
23
 
7,938
122,470
Capacity passengers (per.)
1
 
98
400
Speeds
Max. Speed (km/h)
25
 
390
28,165
Сruise Speed (km/h)
52
 
600
3,087
Fuel
Fuel Capacity (l)
23
 
20,895
320,000
Power
Total Power (hp)
0.4
 
15,020
60,000
4 powerplants 3755 hp each
Performance
Service ceiling (m)
0.6
 
9,753.6
161,544
Range (Ferry range) (km)
4
 
3,540
40,700
with maximum payload
4
 
4,455
40,700
with 7938 kg payload
Dynamic Performance
Rate of climb (m/min)
1.9
 
600.5
36,000
Stat
Number built (qt)
0
 
170
43,000
Introduction 1959
First flight 06.12.1957

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