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    • Year
      1906
      2018
    • Length
      27 m
      42 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      203 m2
      305 m2
    • Wingspan (Beam)
      40 m
      61 m
    • Wing loading
      167 kg/m2
      251 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
      31600 kg
      47400 kg
    • Max. takeoff weight (Gross weight)
      60400 kg
      90600 kg
    • Loaded weight
      42489 kg
      63735 kg
    • Crew
      8 per.
      12 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      404 km/h
      606 km/h
    • Сruise Speed
      284 km/h
      426 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
      5440 hp
      8160 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      7760 km
      11640 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
      1 m/min
      36000 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
      5 qt
      9 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 390

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
34.2
88.7
Height (m)
0.6
 
6.9
50.1
Wings
Wing area (m2)
1.1
 
254
925
Wingspan (Beam) (m)
0.1
 
50.3
95
Wing loading (kg/m2)
3.1
 
209
829
Weights
Empty weight (kg)
8
 
39,500
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
75,500
575,000
Loaded weight (kg)
5
 
53,112
242,500
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
505
28,165
Сruise Speed (km/h)
52
 
355
3,087
Power
Total Power (hp)
0.4
 
6,800
60,000
4 powerplants 1700 hp each
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Range (Ferry range) (km)
4
 
9,700
40,700
Combat
Guns (qt)
1
 
7
18
2 × 20 mm MG 151/20 cannons in dorsal turrets; 1 × 20 mm MG 151/20 in tail; 2 × 13 mm (.51 in) MG 131 machine guns at waist; 2 × 13 mm (.51 in) MG 131s in gondola
Stat
Number built (qt)
0
 
2
43,000
Introduction 1943
First flight 20.10.1943
Stop production 1945

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