Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      49 m2
      74 m2
    • Wingspan (Beam)
      15 m
      24 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
      2792 kg
      4188 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      4392 kg
      6588 kg
    • Crew
      1 per.
      112 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
      232 km/h
      348 km/h
    • Сruise Speed
      52 km/h
      3087 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
      664 hp
      996 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5360 m
      8040 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
      148 m/min
      224 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
      480 kg
      720 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      123 qt
      185 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.111

TypeAircraft
Company

Caproni

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
15.3
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
61.5
925
Wingspan (Beam) (m)
0.1
 
19.7
95
Weights
Empty weight (kg)
8
 
3,490
276,800
Loaded weight (kg)
5
 
5,490
242,500
Speeds
Max. Speed (km/h)
25
 
290
28,165
Power
Total Power (hp)
0.4
 
830
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,700
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
186
36,000
Combat
Guns (qt)
1
 
4
18
7.7 mm (.303 in) Breda-SAFAT machine gun in flexible positions in dorsal, ventral, and beam positions
Bombs weight (kg)
2
 
600
39,000
Stat
Number built (qt)
0
 
154
43,000
152 + 2 prototypes
Introduction 1932
First flight 01.02.1932

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