Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      44 m2
      68 m2
    • Wingspan (Beam)
      17 m
      27 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
      8320 kg
      12480 kg
    • Max. takeoff weight (Gross weight)
      11740 kg
      17610 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      330 km/h
      496 km/h
    • Max. Speed
      492 km/h
      740 km/h
    • Сruise Speed
      448 km/h
      672 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
      2896 hp
      4344 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10752 m
      16128 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      302 m/min
      454 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
      80 qt
      120 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 388

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16.3
88.7
Height (m)
0.6
 
4.4
50.1
Wings
Wing area (m2)
1.1
 
56
925
Wingspan (Beam) (m)
0.1
 
22
95
Weights
Empty weight (kg)
8
 
10,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,675
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Ground Speed (km/h)
96.6
 
413
1,500
Max. Speed (km/h)
25
 
616
28,165
Сruise Speed (km/h)
52
 
560
3,087
Power
Total Power (hp)
0.4
 
3,620
60,000
2 powerplants 1810 hp each
Performance
Service ceiling (m)
0.6
 
13,440
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
378
36,000
Stat
Number built (qt)
0
 
100
43,000
Introduction 1943
First flight 22.12.1943
Stop production 1945

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