Fiat G.80

Fiat G.80

__NOTOC__ Infobox Aircraft
name=G.80 and G.82


caption=
type=Trainer
manufacturer=Fiat
designer=Giuseppe Gabrielli
first flight=9 December avyear|1951
introduced=
retired=
status=
primary user=
more users=
produced=
number built=10
variants with their own articles=
The Fiat G.80 was a military trainer aircraft developed in Italy in the 1950s, and was that country's first true jet-powered aircraft. It was a conventional low-wing monoplane with retractable tricycle undercarriage and engine intakes on the fuselage sides. The pilot and instructor sat in tandem under a long bubble canopy.

Two G.80 prototypes were followed by three pre-production machines, but the Aeronautica Militare found it unsuitable to their requirements and did not purchase it in quantity. Undeterred, Fiat developed a refined version dubbed the G.82 for entry in a NATO competition to select a standard jet trainer. Apart from many detail changes, the G.82 featured a longer fuselage, a Rolls-Royce Nene engine in place of the G.80's de Havilland Goblin, and tip tanks. Five aircraft were constructed, but when the competition was cancelled and the G.82 was not selected by either NATO or the Aeronautica Militare, the development programme was finally terminated. Plans for specialised versions including nightfighter, reconnaissance, and close-support aircraft went unrealised, as did the G.84 that was to have been powered by an Allison J35. The G.82s were used for a few years by the Aeronautica Militare's training school at Amendola before being handed over to the Reparto Sperimentale Volo ("Department of Experimental Flight") in 1957.

Variants

* G.80-1B - prototype (1 built)
* G.80-3B - pre-production version (4 built)
* G.81 - definitive production version of G.80 (not built, development cancelled in favour of G.82)
* G.82 - prototypes for NATO competition (5 built)
* G.84 - Allison J35-powered version (not built)

Operators

;ITA
*Italian Air Force

pecifications (G.82)

aerospecs
ref=
met or eng?= met

crew=Two, pilot and instructor
capacity=
length m=12.93
length ft=42
length in=5
span m=11.80
span ft=38
span in=9
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=4.07
height ft=13
height in=4
wing area sqm=26.0
wing area sqft=280
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=4,400
empty weight lb=9,700
gross weight kg=6,250
gross weight lb=13,880
lift kg=
lift lb=

eng1 number=1
eng1 type=Rolls-Royce Nene 6/21
eng1 kw=
eng1 hp=
eng1 kn= 24.0
eng1 lbf= 5,390
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=910
max speed mph=570
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,150
range miles=710
endurance h=
endurance min=
ceiling m=12,300
ceiling ft=40,400
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=2 × fixed, forward-firing .50 Colt-Browning M3 machine guns
armament2=Up to 340 kg (750 lb) of disposable stores on two pylons, including bombs or rockets
armament3=
armament4=
armament5=
armament6=

aircontent
see also=
related=
similar aircraft=
lists=

References

*
* [http://www.aeronautica.difesa.it/sitoam/images/G80%20TESTO-FOTO%20ALL%20IN%20ONE.pdf Italian Defence Department fact sheet] (PDF format)
* [http://www.airwar.ru/enc/attack/g82.html Уголок неба]


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