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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      160 m2
      240 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
      5367 kg
      8051 kg
    • Max. takeoff weight (Gross weight)
      6000 kg
      9000 kg
    • Loaded weight
      5 kg
      242500 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
      112 km/h
      168 km/h
    • Сruise Speed
      86 km/h
      130 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
      960 hp
      1440 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2400 m
      3600 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
      5 h
      9 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
      99 m/min
      150 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1160 kg
      1740 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      42 qt
      64 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.4

TypeAircraft
Company

Caproni

Scheme

Triplane

Geometry
Length (m)
1.9
 
13.1
88.7
Height (m)
0.6
 
6.3
50.1
Wings
Wing area (m2)
1.1
 
200
925
Wingspan (Beam) (m)
0.1
 
29.9
95
Weights
Empty weight (kg)
8
 
6,709
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,500
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, co-pilot, front gunner, and rear gunner/mechanic
Speeds
Max. Speed (km/h)
25
 
140
28,165
Сruise Speed (km/h)
52
 
108
3,087
Power
Total Power (hp)
0.4
 
1,200
60,000
3 powerplants 400 hp each
Performance
Service ceiling (m)
0.6
 
3,000
161,544
Endurance (h)
0.0
 
7
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
124.8
36,000
Combat
Guns (qt)
1
 
4
18
6.5 mm FIAT-Revelli machine guns, two in forward mounting and one in each of two rearward positions
Bombs weight (kg)
2
 
1,450
39,000
Stat
Number built (qt)
0
 
53
43,000
Introduction 1916
First flight 1917

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