Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      48 m2
    • Wingspan (Beam)
      15 m
      23 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
      2 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
      2560 kg
      3840 kg
    • Max. takeoff weight (Gross weight)
      4240 kg
      6360 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      260 km/h
      390 km/h
    • Сruise Speed
      236 km/h
      354 km/h
    • Stall Speed
      88 km/h
      132 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
      600 hp
      900 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5040 m
      7560 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      2 qt
      4 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.124

TypeAircraft
Company

Caproni

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
13.8
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
40
925
Wingspan (Beam) (m)
0.1
 
18.9
95
Rotors
Rotor number (qt)
1
 
1
8
Weights
Empty weight (kg)
8
 
3,200
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,300
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
325
28,165
Сruise Speed (km/h)
52
 
295
3,087
Stall Speed (km/h)
40
 
110
257.7
Power
Total Power (hp)
0.4
 
750
60,000
Performance
Service ceiling (m)
0.6
 
6,300
161,544
Propellers
Prop blade number (qt)
1
 
3
8
Stat
Number built (qt)
0
 
1
43,000
Introduction 1934
First flight 1937

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