AgustaWestland AW609

	Attribution Attribution	Overview Parent type *No type assigned Variant *No Variant assigned Design authority AgustaWestland N.V. Primary manufacturer AgustaWestland N.V. Key Characteristics Operational status In development Max gross weight (ground) 7,620 n/a 7,620 n/a Crew 2 Seating arrangement Side-by-side Configuration VTOL type Convertiplane Compound type N/A Lift configuration Tilt rotor/prop Control device type None Features Number of engines 2 Number of propulsors 0 Number of lift devices 2 Number of control devices 0 Milestones associated with the AgustaWestland AW609 2003 First flight of the BA609 tilt rotor

AgustaWestland AW609

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AgustaWestland AW609

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AgustaWestland AW609

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AgustaWestland AW609

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AgustaWestland AW609

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AgustaWestland AW609

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AgustaWestland AW609

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Articles from the Journal of the American Helicopter Society related to the AgustaWestland AW609

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Articles from NASA Technical Reports Server related to the AgustaWestland AW609

 

Patent information from the US Patent and Trademark Office related to the AgustaWestland AW609

 

Google Books related to the AgustaWestland AW609

AgustaWestland AW609

Overview

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AgustaWestland AW609

Aircraft Notes