Alenia ITV

__NOTOC__ Infobox Aircraft
name=ITV


caption=
type=Technology demonstrator
national origin=
manufacturer=Alenia
designer=
first flight=
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
variants with their own articles=

The Alenia ITV is a technology demonstrator aircraft developed in Italy in the early 21st century. In the spring of 2003, Alenia Aeronautica of Italy unveiled a non-flying ground-test prototype of a half-scale UCAV demonstrator, known as an "Integration Technology Vehicle (ITV)", with a flight prototype to follow. The ITV has a high-mounted wing with a sweep of 35 degrees; a vee tail; a Microturbo TRI60-5 turbojet, with 4.4 kN (450 kgp / 990 lbf) thrust, mounted on the back behind the wing; retractable tricycle landing gear; and metal construction.

As the ITV designation suggests, this machine is strictly for technology development and risk reduction. A "real" Alenia Aeronautica UCAV will be at least twice as big, use a tailless delta configuration, and will be made mostly of composite materials. It will have a modular payload bay for carriage of smart weapons, SAR, or day-night EO sensors. Alenia Spazio, a sister organization in the Finnmeccia Group, will provide a satellite data link. Meteor is also part of the Finnmeccia group and there is likely some collaboration between Meteor and Alenia Aeronautica on UAV design.

pecifications

aerospecs
ref=
met or eng?= met

crew=None
capacity=300 kg (660 lb) payload
length m=6.00
length ft=19
length in=8
span m=5.74
span ft=18
span in=10
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=
height ft=
height in=
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=550
empty weight lb=1,210
gross weight kg=1,000
gross weight lb=2,200
lift kg=
lift lb=

eng1 number=1
eng1 type=Microturbo TRI60-5
eng1 kw=
eng1 hp=
eng1 kn= 4.4
eng1 lbf= 990
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=
max speed mph=
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=185
range miles=115
endurance h=
endurance min=
ceiling m=10,000
ceiling ft=32,800
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

aircontent
see also=
related=
similar aircraft=
lists=

References

This article contains material that originally came from the web article [http://www.vectorsite.net/twuav.html "Unmanned Aerial Vehicles"] by Greg Goebel, which exists in the Public Domain.