Caproni Ca.132

Caproni Ca.132

__NOTOC__ Infobox Aircraft
name=Ca.132


caption=
type=Bomber/airliner
manufacturer=Caproni
designer=
first flight=1934
introduced=
retired=
status=Prototype only
primary user=
more users=
produced=
number built=
variants with their own articles=

The Caproni Ca.132 was a prototype for a large aircraft built in Italy in 1934, intended for use as either a bomber or airliner. It was a conventional low-wing cantilever monoplane powered by a radial engines on each wing and in the nose. The main undercarriage was housed within large streamlined spats. Configured as an airliner, it would have seated 20 passengers.

pecifications (as bomber)

aerospecs
ref=
met or eng?= met

crew=Four
capacity=
length m=18.60
length ft=61
length in=0
span m=26.69
span ft=87
span in=7
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=4.15
height ft=13
height in=7
wing area sqm=100.9
wing area sqft=1,086
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=7,000
empty weight lb=15,430
gross weight kg=10,700
gross weight lb=23,590
lift kg=
lift lb=

eng1 number=3
eng1 type=Piaggio Stella IX
eng1 kw= 418
eng1 hp= 560
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=314
max speed mph=196
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=6,300
ceiling ft=20,664
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=4 × 7.7 mm Breda-SAFAT machine guns
armament2=900 kg (1,980 lb) of bombs
armament3=
armament4=
armament5=
armament6=

References

*
* [http://www.airwar.ru/enc/bww2/ca132.html Уголок неба]

ee also

aircontent

related=

similar aircraft=

sequence= ← Ca.129 -
Ca.130 -
Ca.131 - Ca.132 -
Ca.133 -
Ca.134 -
Ca.135

lists=

see also=


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