- Development and design
- Variants
- Operators
- Specifications (A.105)
- References
| name=A.105B | image=Agusta A105B MM80416 LEB 19.06.65 edited-2.jpg | caption=Agusta A.105B prototype exhibited at the 1965 Paris Air Show }}{{Infobox Aircraft Type | type=Prototype light helicopter | national origin=Italy | manufacturer=Agusta | designer= | first flight=October 1964 | introduced= | retired= | status= | primary user= | number built=2[1] | developed from= | variants with their own articles=
}} |
The Agusta A.105 was an Italian rotorcraft designed by Agusta. It was never developed beyond the prototype stage. Development and designThe A.105 was designed to simplify the manufacturing process. Built to be a liaison, aerial photography and high-speed transport helicopter, it was powered by the Agusta built Turbomeca-Agusta TA-230 turbine engine. The A.105 and A.105B were displayed at the 1965 Paris Air Show, the latter wearing Italian Air Force markings. Both variants did not progress beyond the prototype stage. Variants- A.105
Original two-seat prototype - A.105B
Four seater variant. Operators- {{ITA}}
Specifications (A.105) {{Aircraft specs
|ref=Jane's All The World's Aircraft 1965-66 [2]
|prime units?=met
|genhide=
|crew=2
|capacity=
|length m=6.72
|length ft=
|length in=
|length note=(fuselage length)
|height m=2.42
|height ft=
|height in=
|empty weight kg=550
|empty weight lb=
|gross weight kg=1150
|gross weight lb=
|max takeoff weight kg=1700
|max takeoff weight lb=
|more general=
|eng1 number=1
|eng1 name=Turbomeca-Agusta TA-230
|eng1 type=turboshaft
|eng1 kw=
|eng1 hp=
|eng1 shp=275
|power original=
|thrust original=
|more power=
|rot number=1
|rot dia m=8.40
|rot dia ft=
|rot dia in=
|rot area sqm=55.4
|rot area sqft=
|perfhide=
|max speed kmh=185
|max speed mph=
|max speed kts=
|cruise speed kmh=175
|cruise speed mph=
|cruise speed kts=
|range km=310
|range miles=
|range nmi=
|endurance=1 hr 45 min
|ceiling m=2800
|ceiling ft=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|lift to drag=
|disk loading kg/m2
|disk loading lb/sqft=
|more performance=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
References{{commons category}}1. ^1 aeroflight
2. ^Taylor 1965, pp. 88–89.
{{refbegin}}- {{cite book|last=Taylor|first=John W. R.|authorlink=John W. R. Taylor |coauthors= |title= Jane's All The World's Aircraft 1965-66 |year=1965 |publisher=Samson Low, Marston |location= London|isbn= |page= |pages= |url= |accessdate=}}
{{refend}}{{AgustaWestland aircraft}} 4 : Italian helicopters 1960–1969|Agusta aircraft|Italian civil utility aircraft 1960–1969|Aircraft first flown in 1964 |