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Aerocrane: A hybrid LTA aircraft for aerial crane applicationsThe Aerocrane, a hybrid aircraft, combines rotor lift with buoyant lift to offer VTOL load capability greatly in excess of helicopter technology while eliminating the airship problem of ballast transfer. In addition, the Aerocrane concept sharply reduces the mooring problem of airships and provides 360 deg vectorable thrust to supply a relatively large force component for control of gust loads. Designed for use in short range, ultra heavy lift missions, the Aerocrane operates in a performance envelope unsuitable for either helicopters or airships. Basic design considerations and potential problem areas of the concept are addressed.
Document ID
19760007975
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perkins, R. G., Jr.
(Naval Air Systems Command Washington, DC, United States)
Doolittle, D. B.
(All Am. Eng. Co.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: MIT Proc. of the Interagency Workshop on Lighter than Air Vehicles
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N15063
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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