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    • 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
      15 m2
      23 m2
    • Wingspan (Beam)
      7 m
      11 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
      436 kg
      654 kg
    • Max. takeoff weight (Gross weight)
      652 kg
      978 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      176 km/h
      264 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      64 km/h
      96 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
      96 l
      144 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
      108 hp
      162 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4400 m
      6600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      720 km
      1080 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
      3 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.125

TypeAircraft
Company

Caproni

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.3
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
19
925
Wingspan (Beam) (m)
0.1
 
8.9
95
Rotors
Rotor number (qt)
1
 
1
8
Weights
Empty weight (kg)
8
 
545
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
815
575,000
Capacity
Capacity passengers (per.)
1
 
2
400
Speeds
Max. Speed (km/h)
25
 
220
28,165
Stall Speed (km/h)
40
 
80
257.7
Fuel
Fuel Capacity (l)
23
 
120
320,000
Power
Total Power (hp)
0.4
 
135
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,500
161,544
Range (Ferry range) (km)
4
 
900
40,700
Propellers
Prop blade number (qt)
1
 
2
8
Stat
Number built (qt)
0
 
2
43,000
First flight 1933

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