Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      79 m2
      119 m2
    • Wingspan (Beam)
      23 m
      36 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
      3464 kg
      5196 kg
    • Max. takeoff weight (Gross weight)
      4800 kg
      7200 kg
    • Loaded weight
      5760 kg
      8640 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      168 km/h
      252 km/h
    • Сruise Speed
      136 km/h
      204 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
      744 hp
      1116 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      528 km
      792 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
      118 m/min
      178 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      10 min
      17 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
      57 qt
      87 qt
    • Price
      41 USD
      750000000 USD

Junkers G 24

TypeAircraft
Company

Junkers Flugzeug- und Motorenwerke AG

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
15.8
88.7
Height (m)
0.6
 
5.8
50.1
Wings
Wing area (m2)
1.1
 
99
925
Wingspan (Beam) (m)
0.1
 
29.4
95
Weights
Empty weight (kg)
8
 
4,330
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,000
575,000
Loaded weight (kg)
5
 
7,200
242,500
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
14
400
Speeds
Max. Speed (km/h)
25
 
210
28,165
Сruise Speed (km/h)
52
 
170
3,087
Power
Total Power (hp)
0.4
 
930
60,000
3 powerplants 310 hp each (1 powerplant for F 24)
Performance
Service ceiling (m)
0.6
 
4,000
161,544
with maximum payload
Range (Ferry range) (km)
4
 
660
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
148.2
36,000
Time to altitude (min)
0.6
 
13.5
105
to 2000 m
Stat
Number built (qt)
0
 
72
43,000
Introduction 1925
First flight 19.09.1924

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