AgustaWestland A129 Mangusta

	Attribution Attribution	Overview Parent type A129/AW129 Variant *No Variant assigned Design authority AgustaWestland N.V. Primary manufacturer AgustaWestland N.V. Key Characteristics Operational status Operational Max gross weight (ground)   109 4,100 n/a 4,100 n/a Crew 2 Seating arrangement Tandem Configuration VTOL type Helicopter Compound type None Lift configuration Single main rotor Control device type Tail rotor Features Number of engines 2 Number of propulsors 0 Number of lift devices 1 Number of control devices 1 Milestones associated with the AgustaWestland A129 Mangusta 1983 First flight of the Agusta A.129 Mangusta (Mongoose)

AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

AgustaWestland A129 Mangusta

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Articles from the Journal of the American Helicopter Society related to the AgustaWestland A129

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Articles from NASA Technical Reports Server related to the AgustaWestland A129

 

Patent information from the US Patent and Trademark Office related to the AgustaWestland A129

 

Google Books related to the AgustaWestland A129

AgustaWestland A129 Mangusta

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AgustaWestland A129 Mangusta

Aircraft Notes