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    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      72 m2
    • Wingspan (Beam)
      14 m
      22 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
      5084 kg
      7626 kg
    • Max. takeoff weight (Gross weight)
      7484 kg
      11226 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 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
      308 km/h
      464 km/h
    • Сruise Speed
      273 km/h
      411 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
      1320 hp
      1980 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5800 m
      8700 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1560 km
      2340 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      15 min
      24 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      4 qt
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1280 kg
      1920 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      23 qt
      35 qt
    • Price
      41 USD
      750000000 USD

Caproni P.32

TypeAircraft
Company

Caproni

Piaggio Aerospace

Scheme

Monoplane

Low wing

Midwing

Geometry
Length (m)
1.9
 
16.3
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
60
925
Wingspan (Beam) (m)
0.1
 
18
95
Weights
Empty weight (kg)
8
 
6,355
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
9,355
575,000
Capacity
Crew (per.)
1
 
6
112
5-6
Speeds
Max. Speed (km/h)
25
 
386
28,165
Сruise Speed (km/h)
52
 
342
3,087
Power
Total Power (hp)
0.4
 
1,650
60,000
2 powerplants 825 hp each
Performance
Service ceiling (m)
0.6
 
7,250
161,544
Range (Ferry range) (km)
4
 
1,950
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
19.9
105
to 5000 m
Combat
Guns (qt)
1
 
5
18
7.7 mm (0.303 in) Breda-SAFAT machine guns
Bombs weight (kg)
2
 
1,600
39,000
Stat
Number built (qt)
0
 
29
43,000
Introduction 1936
First flight 1936
Stop production 1939

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