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Lifting Loads With Two HelicoptersReport discusses theoretical equilibrium characteristics of dual-helicopter lifting system. Analysis presented provides mathematical basis for selection of lifting configurations and flight parameters. Force-balance equations serve as basis for coordination in flight. Employed in both military and civilian sectors to deliver weapons, vehicles, and construction materials.
Document ID
19920000046
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Cicolani, L. S.
(NASA Ames Research Center, Moffett Field, CA.)
Kanning, G.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 1
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-11812
ISSN: 0145-319X
Report Number: ARC-11812
Accession Number
92B10046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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