Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      40 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      96 kg/m2
      144 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
      2091 kg
      3138 kg
    • Max. takeoff weight (Gross weight)
      3338 kg
      5008 kg
    • Loaded weight
      3139 kg
      4709 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      289 km/h
      435 km/h
    • Сruise Speed
      272 km/h
      410 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
      720 hp
      1080 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5583 m
      8376 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1040 km
      1560 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
      341 m/min
      513 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      2 m
      4 m
    • Prop blade number
      1 qt
      3 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
      104 qt
      156 qt
    • Price
      41 USD
      750000000 USD

Lockheed JO Electra Junior

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
32.7
925
Wingspan (Beam) (m)
0.1
 
15.1
95
Wing loading (kg/m2)
3.1
 
120
829
Weights
Empty weight (kg)
8
 
2,615.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,173.1
575,000
Loaded weight (kg)
5
 
3,924
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and co-pilot
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
362
28,165
at 1500 m
Сruise Speed (km/h)
52
 
341
3,087
Power
Total Power (hp)
0.4
 
900
60,000
2 powerplants 450 hp each
Performance
Service ceiling (m)
0.6
 
6,979.9
161,544
Range (Ferry range) (km)
4
 
1,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
427
36,000
Propellers
Propellers (qt)
1
 
2
8
1 per engine
Prop diameter (m)
1.8
 
2.8
5.8
2,6 to 2,75 m
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
130
43,000
Introduction 1936
First flight 27.06.1936

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