Caproni Vizzola Ventura

__NOTOC__ Infobox Aircraft
name=C22 Ventura


caption=
type=Military trainer aircraft
manufacturer=Caproni Vizzola
designer=
first flight=21 July 1980
introduced=
retired=
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produced=
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The Caproni Vizzola C22 Vizzola was a light jet-powered aircraft developed in Italy for use as a military trainer. It was of conventional sailplane configuration and bore a family resemblance to the Caproni's Calif gliders, although the Ventura had an almost entirely metal structure. The student and instructor sat side-by-side under an expansive canopy, and weapons hardpoints were provided under each of the slender, high-mounted wings. Retractable, tricycle undercarriage was fitted.

In 1981, Agusta acquired 50% of the C22 programme and proposed a new version, the C22R, which was to have been a reconnaissance aircraft also capable of Forward Air Control and ELINT operations. The basic C22J trainer failed to attract any customers, and the C22R was never actually built.

pecifications (C22J)

aerospecs
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crew=Two, pilot and instructor
capacity=
length m=6.19
length ft=20
length in=3
span m=10.00
span ft=32
span in=10
swept m=
swept ft=
swept in=
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rot dia m=
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dia m=
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width m=
width ft=
width in=
height m=1.88
height ft=6
height in=2
wing area sqm=8.8
wing area sqft=94
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=720
empty weight lb=1,590
gross weight kg=1,135
gross weight lb=2,500
lift kg=
lift lb=

eng1 number=2
eng1 type=Microturbo TRS 18-046
eng1 kw=
eng1 hp=
eng1 kn= 1.0
eng1 lbf= 220
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max speed kmh=
max speed mph=
max speed mach=
cruise speed kmh= 482
cruise speed mph= 299
range km=740
range miles=460
endurance h=
endurance min=
ceiling m=7,600
ceiling ft=24,930
glide ratio=
climb rate ms=9.1
climb rate ftmin=1,810
sink rate ms=
sink rate ftmin=

armament1=Up to 250 kg (551 lb) in disposable stores
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References

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