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
      65 m2
      99 m2
    • Wingspan (Beam)
      25 m
      39 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
      5360 kg
      8040 kg
    • Max. takeoff weight (Gross weight)
      9224 kg
      13836 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      240 km/h
      360 km/h
    • Max. Speed
      336 km/h
      504 km/h
    • Сruise Speed
      228 km/h
      342 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
      1600 hp
      2400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      10400 m
      15600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1264 km
      1896 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      452 km
      678 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
      224 m/min
      337 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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      800 kg
      1200 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 86

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
16.5
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
82
925
Wingspan (Beam) (m)
0.1
 
32
95
Weights
Empty weight (kg)
8
 
6,700
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,530
575,000
Capacity
Crew (per.)
1
 
2
112
pilot and radio operator
Speeds
Ground Speed (km/h)
96.6
 
300
1,500
Max. Speed (km/h)
25
 
420
28,165
above 9150 m
Сruise Speed (km/h)
52
 
285
3,087
Power
Total Power (hp)
0.4
 
2,000
60,000
2 powerplant 1000 hp each
Performance
Service ceiling (m)
0.6
 
13,000
161,544
Range (Ferry range) (km)
4
 
1,580
40,700
Сombat radius (km)
277
 
565
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
280.2
36,000
Combat
Guns (qt)
1
 
3
18
MG 15 machine guns
Bombs weight (kg)
2
 
1,000
39,000
Stat
Introduction 1940
First flight 1934

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