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    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      43 m2
      66 m2
    • Wingspan (Beam)
      16 m
      24 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
      8864 kg
      13296 kg
    • Max. takeoff weight (Gross weight)
      11200 kg
      16800 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      290 km/h
      436 km/h
    • Max. Speed
      346 km/h
      520 km/h
    • Сruise Speed
      280 km/h
      420 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
      2240 hp
      3360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7200 m
      10800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1944 km
      2916 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      824 km
      1236 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
      188 m/min
      282 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
      4 qt
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2400 kg
      3600 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      12146 qt
      18220 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 88

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
14.9
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
54.7
925
Wingspan (Beam) (m)
0.1
 
20
95
Weights
Empty weight (kg)
8
 
11,080
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,000
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, bombardier/front gunner, radio operator/rear gunner, navigator/ventral gunner
Speeds
Ground Speed (km/h)
96.6
 
363
1,500
Max. Speed (km/h)
25
 
510
28,165
at 5300 m without external bomb racks
25
 
433
28,165
at 4500 m at 14000 kg
Сruise Speed (km/h)
52
 
350
3,087
Power
Total Power (hp)
0.4
 
2,800
60,000
2 powerplants 1400 hp each
Performance
Service ceiling (m)
0.6
 
9,000
161,544
at average weight, without bombs
Range (Ferry range) (km)
4
 
2,430
40,700
maximum internal fuel
Сombat radius (km)
277
 
1,030
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
235
36,000
Combat
Guns (qt)
1
 
5
18
1 × 7.92 mm MG 81J machine gun on flexible mount in front windscreen; 1 × 7.92 mm MG 81J machine gun on flexible mount in lower fuselage nose glazing; 2 × 7.92 mm MG 81J machine guns on flexible mount in the rear of the cockpit canopy; 1 × 7.92 mm MG 81Z twin machine gun on flexible mount in the rear ventral Bola position
Bombs weight (kg)
2
 
1,400
39,000
of ordnance internally or
2
 
3,000
39,000
externally
Stat
Number built (qt)
0
 
15,183
43,000
Introduction 1942
First flight 21.12.1936
Stop production 1951

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