Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      48 m2
    • Wingspan (Beam)
      14 m
      22 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
      1720 kg
      2580 kg
    • Max. takeoff weight (Gross weight)
      2180 kg
      3270 kg
    • Loaded weight
      2784 kg
      4176 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
      96 km/h
      1500 km/h
    • Max. Speed
      184 km/h
      276 km/h
    • Сruise Speed
      156 km/h
      234 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
      480 hp
      720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      664 km
      996 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
      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
      80 kg
      120 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Junkers A 32

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.1
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
40
925
Wingspan (Beam) (m)
0.1
 
17.8
95
Weights
Empty weight (kg)
8
 
2,150
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,725
575,000
Loaded weight (kg)
5
 
3,480
242,500
Capacity
Crew (per.)
1
 
4
112
pilot, oberver, gunner, and bombardier
Speeds
Max. Speed (km/h)
25
 
230
28,165
Сruise Speed (km/h)
52
 
195
3,087
Power
Total Power (hp)
0.4
 
600
60,000
1 powerplant
Performance
Range (Ferry range) (km)
4
 
830
40,700
Combat
Guns (qt)
1
 
3
18
2 × fixed, forward-firing machine guns; 1 × trainable, rearward-firing machine gun
Bombs weight (kg)
2
 
100
39,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1926
First flight 1926

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