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==Specifications (A.105) ==
==Specifications (A.105) ==
{{Aircraft specs
{{aerospecs
|ref=aviastar.com<ref name="aviastar"/>
|ref=aviastar.com<ref name="aviastar"/>
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
|met or eng?=met
<!--
General characteristics
-->
|genhide=


|crew=1
|crew=1
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|length ft=
|length ft=
|length in=
|length in=
⚫
|dia m=<!-- airships etc -->
|span m=
|dia ft=<!-- airships etc -->
|span ft=
|dia in=<!-- airships etc -->
|span in=
|width m=<!-- if applicable -->
|rot number=1
|width ft=<!-- if applicable -->
⚫
|rot dia m=9.00
|rot dia ft=<!-- helicopters -->
|width in=<!-- if applicable -->
⚫
|rot dia in=<!-- helicopters -->
|height m=2.60
|height m=2.60
|height ft=
|height ft=
|height in=
|height in=
|wing area sqm=
|wing area sqft=
⚫
|rot area sqm=<!-- helicopters -->
⚫
|rot area sqft=<!-- helicopters -->
|empty weight kg=485
|empty weight kg=485
|empty weight lb=
|empty weight lb=
|gross weight kg=1000
|gross weight kg=1000
|gross weight lb=
|gross weight lb=
|max takeoff weight kg=

|max takeoff weight lb=
|more general=
<!--
Powerplant
-->
|eng1 number=1
|eng1 number=1
|eng1 type=[[Turbomeca-Agusta TA-230]] turbine
|eng1 name=[[Turbomeca-Agusta TA-230]]
|eng1 kw=261
|eng1 type=[[turboshaft]]
|eng1 hp=350
|eng1 kw=260<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng2 number=
|eng1 shp=<!-- prop engines -->
|eng2 type=
|eng2 kw=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng2 hp=<!-- prop engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|power original=
|thrust original=
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|more power=

|rot number=1<!-- helicopters -->
⚫
|rot dia m=9.00<!-- helicopters -->
|rot dia ft=<!-- helicopters -->
|rot dia in=<!-- helicopters -->
⚫
|rot area sqm=<!-- helicopters -->
⚫
|rot area sqft=<!-- helicopters -->
<!--
Performance
-->
|perfhide=


|max speed kmh=
|max speed kmh=
|max speed mph=
|max speed mph=
|cruise speed kmh=210
|max speed kts=
⚫
|cruise speed kmh=210<!-- if max speed unknown -->
|cruise speed mph=<!-- if max speed unknown -->
|cruise speed mph=<!-- if max speed unknown -->
|cruise speed kts=
|stall speed kmh=<!-- aerobatic and STOL aircraft -->
|stall speed mph=<!-- aerobatic and STOL aircraft -->
|range km=320
|range km=320
|range miles=
|range miles=
|range nmi=
⚫
|endurance h=<!-- if range unknown -->
|endurance min=<!-- if range unknown -->
|endurance=<!-- if range unknown -->
|ceiling m=4750
|ceiling m=4750
|ceiling ft=
|ceiling ft=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate ms=
|climb rate ftmin=
|climb rate ftmin=
|lift to drag=
|disk loading kg/m2
|disk loading lb/sqft=
|more performance=


|avionics=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}
}}


Revision as of 13:57, 16 November 2009

A.105
Role Prototype light helicopter
National origin Italy
Manufacturer Agusta
First flight October 1964[1]

The Agusta A.105 was an Italian rotorcraft designed by Agusta. It was never developed beyond the prototype stage.

Development and design

The A.105 was designed to simplify the manufacturing process. Built to be a liaison, aerial photography and high-speed transport, it was powered by the Augusta built Turbomeca-Agusta TA-230 turbine engine. The A.105 and A.105B were displayed at the 1965 Paris Air Show, and both never progressed beyond the prototype stage.[1]

Variants

A.105
Original two-seat prototype
A.105B
Four seater variant.

Specifications (A.105)

Data from aviastar.com[1]

General characteristics

  • Crew: 1
  • Capacity: 2
  • Height: 2.60 m (8 ft 6 in)
  • Empty weight: 485 kg (1,069 lb)
  • Gross weight: 1,000 kg (2,205 lb)
  • Powerplant: 1 × Turbomeca-Agusta TA-230 turboshaft, 260 kW (350 hp)
  • Main rotor diameter: 9.00 m (29 ft 6 in)

Performance

  • Cruise speed: 210 km/h (130 mph, 110 kn)
  • Range: 320 km (200 mi, 170 nmi)
  • Service ceiling: 4,750 m (15,580 ft)

References

  1. ^ a b c Starostin, Maksim. "Agusta A.105 helicopter - development history, photos, technical data". All the world's helicopters and rotorcrafts. aviastar.org. Retrieved 16 November 2009. {{cite web}}: Cite has empty unknown parameter: |month= (help)
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