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    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      62 m2
    • Wingspan (Beam)
      15 m
      24 m
    • Wing loading
      110 kg/m2
      167 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
      3900 kg
      5852 kg
    • Max. takeoff weight (Gross weight)
      6350 kg
      9526 kg
    • Loaded weight
      5679 kg
      8519 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      321 km/h
      483 km/h
    • Сruise Speed
      276 km/h
      416 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
      1952 l
      2928 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1440 hp
      2160 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5974 m
      8962 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1096 km
      1644 km
    • Range PTB (Ferry range)
      2736 km
      4104 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
      369 m/min
      555 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
      283 qt
      425 qt
    • Price
      41 USD
      750000000 USD

Lockheed C-111 Super Electra

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.5
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
51.2
925
Wingspan (Beam) (m)
0.1
 
20.0
95
Wing loading (kg/m2)
3.1
 
138.7
829
3.1
 
138.7
829
Weights
Empty weight (kg)
8
 
4,876.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,938
575,000
Loaded weight (kg)
5
 
7,099
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
14
400
or 12
Speeds
Max. Speed (km/h)
25
 
402.3
28,165
at 1800 m
Сruise Speed (km/h)
52
 
346.0
3,087
Fuel
Fuel Capacity (l)
23
 
2,440
320,000
Power
Power/mass (hp/kg)
0.0
 
0.3
22.1
Total Power (hp)
0.4
 
1,800
60,000
2 powerplants 900 hp each
Performance
Service ceiling (m)
0.6
 
7,468
161,544
Range (Ferry range) (km)
4
 
1,370
40,700
Range PTB (Ferry range) (km)
720
 
3,420
10,000
Dynamic Performance
Rate of climb (m/min)
1.9
 
462
36,000
Stat
Number built (qt)
0
 
354
43,000
Introduction 1937
First flight 29.07.1937

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