Agusta A.104

__NOTOC__ Infobox Aircraft
name=A.104 Helicar


caption=
type=Light helicopter
manufacturer=Agusta
designer=
first flight=1960
introduced=
retired=
status=
primary user=
more users=
produced=
number built=3
variants with their own articles=

The Agusta A.104 Helicar was an Italian prototype light helicopter flown in December 1960. It was a slightly enlarged version of the A.103, and added a second seat beside the pilot's seat. The cockpit was enclosed by a perspex bubble with the engine at the rear and the tail rotor carried on an enclosed boom.

Two piston-engined prototyes were built, followed by a single example of a turbine-engined variant designated A.104BT. No production resulted.

pecifications

aerospecs
met or eng?= met

crew=one, pilot
capacity=1 passenger
length m=6.35
length ft=20
length in=10
span m=
span ft=
span in=
rot number= 1
rot dia m= 7.95
rot dia ft= 26
rot dia in= 1
height m=2.35
height ft=7
height in=8
wing area sqm=
wing area sqft=
rot area sqm= 49.6
rot area sqft= 534
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=640
gross weight lb=1,400

eng1 number=1
eng1 type=Agusta GA.140 (derated)
eng1 kw= 104
eng1 hp= 140
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=165
max speed mph=100
range km=330
range miles=200
endurance h=
ceiling m=3,000
ceiling ft=9,800
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

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External links

* [http://www.luftfahrt-archiv.de/Flugzeugtypen.asp?Type=Link&ID=T1311&Name=A_104_Helicar&SID=384204425 luftfahrt-archiv.de]