Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      47 m2
    • Wingspan (Beam)
      13 m
      20 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
      3679 kg
      5520 kg
    • Max. takeoff weight (Gross weight)
      5480 kg
      8220 kg
    • Loaded weight
      5440 kg
      8161 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      3 qt
    • Ground Speed
      328 km/h
      492 km/h
    • Max. Speed
      404 km/h
      607 km/h
    • Сruise Speed
      360 km/h
      540 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
      1344 hp
      2016 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6480 m
      9720 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1264 km
      1896 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
      336 m/min
      504 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      7 min
      12 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 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
      880 kg
      1320 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

Caproni Ca.331

TypeAircraft
Company

Caproni

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.7
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
38.5
925
Wingspan (Beam) (m)
0.1
 
16.4
95
Weights
Empty weight (kg)
8
 
4,599.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,850
575,000
Loaded weight (kg)
5
 
6,800.3
242,500
Capacity
Crew (per.)
1
 
3
112
Hardpoints (qt)
1
 
2
2,576
for 2 bombs or underwing tanks
Speeds
Ground Speed (km/h)
96.6
 
410
1,500
Max. Speed (km/h)
25
 
505.3
28,165
Сruise Speed (km/h)
52
 
450
3,087
Power
Total Power (hp)
0.4
 
1,680
60,000
2 powerplants 840 hp each
Performance
Service ceiling (m)
0.6
 
8,100
161,544
Range (Ferry range) (km)
4
 
1,580
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
420
36,000
Time to altitude (min)
0.6
 
9.6
105
to 3999 m
Combat
Bombs weight (kg)
2
 
1,100
39,000
1000 kg in bomb bay and 100 on hardpoints
Stat
Number built (qt)
0
 
3
43,000
Introduction 1940
First flight 31.08.1940

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