Agusta A.105: Difference between revisions
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==Development and design== |
==Development and design== |
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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 |
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.<ref name="aviastar"/> |
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Revision as of 03:41, 8 April 2009
| A.105 | |
|---|---|
| Role | liaison/aerial photography/high-speed transport rotorcraft |
| National origin | Italy |
| 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
- 105
- Original prototype
- 105B
- Four seater variant.
Specifications (A.105)
Data from aviastar.com[1]
General characteristics
- Crew: 1
- Capacity: 2
Performance
References
- ^ a b c aviastar.org. Accessed 7 April 2009.