Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      31 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
      1048 kg
      1572 kg
    • Max. takeoff weight (Gross weight)
      1328 kg
      1992 kg
    • Loaded weight
      1328 kg
      1992 kg
    • Crew
      1 per.
      2 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
      284 km/h
      426 km/h
    • Сruise Speed
      244 km/h
      366 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
      424 hp
      636 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7600 m
      11400 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
      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
      600 m/min
      900 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
      3 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
      28 qt
      44 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.114

TypeAircraft
Company

Caproni

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.7
88.7
Height (m)
0.6
 
2.5
50.1
Wings
Wing area (m2)
1.1
 
25.7
925
Wingspan (Beam) (m)
0.1
 
10.5
95
Weights
Empty weight (kg)
8
 
1,310
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,660
575,000
Loaded weight (kg)
5
 
1,660
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
355
28,165
Сruise Speed (km/h)
52
 
305
3,087
Power
Total Power (hp)
0.4
 
530
60,000
at 4000 m 1 powerplant
Performance
Service ceiling (m)
0.6
 
9,500
161,544
Range (Ferry range) (km)
4
 
600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
750
36,000
Combat
Guns (qt)
1
 
2
18
fixed, forward-firing 7.7 mm (.303 in) Breda-SAFAT machine guns
Stat
Number built (qt)
0
 
36
43,000
Introduction 1933
First flight 1933

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