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    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      70 m2
      106 m2
    • Wingspan (Beam)
      25 m
      38 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
      16800 kg
      25200 kg
    • Max. takeoff weight (Gross weight)
      28800 kg
      43200 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
      96 km/h
      1500 km/h
    • Max. Speed
      552 km/h
      828 km/h
    • Сruise Speed
      52 km/h
      3087 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
      8000 hp
      12000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9080 m
      13620 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2716 km
      4074 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
      440 m/min
      662 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      4000 kg
      6000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 488

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Concept

Geometry
Length (m)
1.9
 
23.3
88.7
Height (m)
0.6
 
6.1
50.1
Wings
Wing area (m2)
1.1
 
88
925
Wingspan (Beam) (m)
0.1
 
31.3
95
Weights
Empty weight (kg)
8
 
21,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
36,000
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
690
28,165
at 7200 m
Power
Total Power (hp)
0.4
 
10,000
60,000
4 powerplants 2500 hp of take-off power each
Performance
Service ceiling (m)
0.6
 
11,350
161,544
Range (Ferry range) (km)
4
 
3,395
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
551
36,000
Combat
Guns (qt)
1
 
4
18
2 × 20 mm MG 151 cannons in Fernbedienbare Drehlafette FDL 151Z remotely operated dorsal turret, and 2 × 13 mm (.51 in) MG 131 machine guns in Hecklafette HDL 131Z remote tail turret
Bombs weight (kg)
2
 
5,000
39,000
of disposable stores in internal bay
Stat
Number built (qt)
0
 
2
43,000

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