Search filter

    • Year
      1906
      2018
    • Length
      21 m
      32 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      147 m2
      221 m2
    • Wingspan (Beam)
      28 m
      43 m
    • Wing loading
      89 kg/m2
      135 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
      13600 kg
      20400 kg
    • Max. takeoff weight (Gross weight)
      22240 kg
      33360 kg
    • Loaded weight
      16640 kg
      24960 kg
    • Crew
      4 per.
      6 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
      277 km/h
      417 km/h
    • Max. Speed
      308 km/h
      464 km/h
    • Сruise Speed
      250 km/h
      376 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5600 m
      8400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2384 km
      3576 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
      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
      1280 kg
      1920 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 89

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
26.5
88.7
Height (m)
0.6
 
7.6
50.1
Wings
Wing area (m2)
1.1
 
184
925
Wingspan (Beam) (m)
0.1
 
35.3
95
Wing loading (kg/m2)
3.1
 
112
829
Weights
Empty weight (kg)
8
 
17,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
27,800
575,000
Loaded weight (kg)
5
 
20,800
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Ground Speed (km/h)
96.6
 
347
1,500
Max. Speed (km/h)
25
 
386
28,165
Сruise Speed (km/h)
52
 
313
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
4 powerplants 750 hp each
Performance
Service ceiling (m)
0.6
 
7,000
161,544
Range (Ferry range) (km)
4
 
2,980
40,700
Combat
Guns (qt)
1
 
4
18
2 × 20 mm MG FF cannons; 2 × 7.92 mm (.312 in) MG 15 machine guns
Bombs weight (kg)
2
 
1,600
39,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1936
First flight 11.04.1937
Stop production 1939

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