Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      41 m2
      63 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
      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
      1960 kg
      2940 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      3160 kg
      4740 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      1200 kg
      1800 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      168 km/h
      252 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
      480 hp
      720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4000 m
      6000 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
      124 m/min
      188 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
      32 qt
      48 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
      43000 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.101

TypeAircraft
Company

Caproni

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
13.5
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
52
925
Wingspan (Beam) (m)
0.1
 
18.8
95
Weights
Empty weight (kg)
8
 
2,450
276,800
Loaded weight (kg)
5
 
3,950
242,500
Capacity
Payload (kg)
23
 
1,500
122,470
Speeds
Max. Speed (km/h)
25
 
210
28,165
Power
Total Power (hp)
0.4
 
600
60,000
3 powerplants 200 hp each
Performance
Service ceiling (m)
0.6
 
5,000
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
156
36,000
Combat
Guns (qt)
1
 
2
18
7.7 mm (.303 in) Lewis Guns in the nose and ventral position
Bombs (qt)
1
 
250
250
2 kg or
1
 
40
250
12 kg bombs carried internally
Stat
Introduction 1930
First flight 1928
Stop production 1939

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