Agusta A.103

Infobox Aircraft
name= A.103


caption=
type= Light helicopter
manufacturer= Agusta
designer=
first flight= 1959
introduced=
retired=
status=
primary user=
more users=
produced=
number built1
variants with their own articles=

The Agusta A.103 was an Italian prototype single-seat light helicopter flown in October 1959. The pilot was enclosed by a perspex bubble with the engine at the rear and the tail rotor carried on an enclosed boom.

pecifications

aerospecs
met or eng?= met

crew=one, pilot
capacity=
length m=6.13
length ft=20
length in=1
span m=
span ft=
span in=
rot number= 1
rot dia m= 7.4
rot dia ft= 24
rot dia in= 3
height m=2.3
height ft=7
height in=7
wing area sqm=
wing area sqft=
rot area sqm= 43
rot area sqft= 463
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=460
gross weight lb=1,000

eng1 number=1
eng1 type=Agusta GA.70
eng1 kw= 64
eng1 hp= 85
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=150
max speed mph=90
range km=450
range miles=280
endurance h=
ceiling m=2,000
ceiling ft=6,600
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

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

ee also

aircontent

related=

similar aircraft=

lists=

see also=

References

*
*

External links

* [http://www.luftfahrt-archiv.de/Flugzeugtypen.asp?Type=Link&ID=T1310&Name=A_103&SID=384204425 luftfahrt-archiv.de]