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    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      11 m
      17 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
      2564 kg
      3846 kg
    • Max. takeoff weight (Gross weight)
      4000 kg
      6000 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
      270 km/h
      406 km/h
    • Max. Speed
      312 km/h
      468 km/h
    • Сruise Speed
      268 km/h
      404 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
      480 km/h
      720 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
      947 hp
      1421 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6560 m
      9840 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      400 km
      600 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      480 km
      720 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
      266 m/min
      400 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      2 m
      5 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      4 qt
      6 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
      5200 qt
      7800 qt
    • Price
      41 USD
      750000000 USD

Junkers Ju 87

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11
88.7
Height (m)
0.6
 
4.2
50.1
Wings
Wing area (m2)
1.1
 
31.9
925
Wingspan (Beam) (m)
0.1
 
13.8
95
Weights
Empty weight (kg)
8
 
3,205
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,000
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
338
1,500
Max. Speed (km/h)
25
 
390
28,165
at 4400 m
Сruise Speed (km/h)
52
 
336
3,087
Never exceed speed (km/h)
108.0
 
600
1,050
Power
Total Power (hp)
0.4
 
1,184
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,200
161,544
with 500 kg bomb load
Range (Ferry range) (km)
4
 
500
40,700
with 500 kg bomb load
Сombat radius (km)
277
 
600
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
333
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
3.4
5.8
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
3
18
2× 7.92 mm (.312 in) MG 17 machine gun forward, 1× 7.92 mm (.312 in) MG 15 machine gun to rear
Bombs (qt)
1
 
5
250
1× 250 kg (550 lb) bomb beneath the fuselage and 4× 50 kg (110 lb), two bombs underneath each wing
Stat
Number built (qt)
0
 
6,500
43,000
Introduction 1936
First flight 17.09.1935
Stop production 1945

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