Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      17 m2
    • Wingspan (Beam)
      8 m
      13 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
      288 kg
      432 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      480 kg
      720 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
      96 km/h
      1500 km/h
    • Max. Speed
      137 km/h
      207 km/h
    • Сruise Speed
      116 km/h
      174 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
      69 hp
      105 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      480 km
      720 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      200 m
      300 m
    • Landing roll
      149 m
      225 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
      1 qt
      18 qt
    • Bombs
      1 qt
      250 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
      55 qt
      83 qt
    • Price
      990 USD
      1487 USD

Junkers A 50 Junior

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
7.1
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
13.7
925
Wingspan (Beam) (m)
0.1
 
10.0
95
Weights
Empty weight (kg)
8
 
360
276,800
Loaded weight (kg)
5
 
600
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
172
28,165
Сruise Speed (km/h)
52
 
145
3,087
Power
Total Power (hp)
0.4
 
86.7
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Range (Ferry range) (km)
4
 
600
40,700
Takeoff roll (m)
20
 
250
3,200
Landing roll (m)
20
 
187
2,570
Stat
Number built (qt)
0
 
69
43,000
Price (USD)
41.5
 
1,238.6
750.0 million
Introduction 1929
First flight 13.02.1929

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