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Deployment and retraction of a cable-driven solar array: Testing and simulationThe paper investigates three critical areas in cable-driven rigid-panel solar arrays: First, the variation of deployment and retraction cable tensions due to friction at the hinges; Second, the change in deployment dynamics associated with different deployment histories; Third, the relationship between the level of pre-tension in the closed contact loops and the synchronization of deployment. A small scale model array has been made and tested, and its behavior has been compared to numerical simulations.
Document ID
19950020863
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kumar, P.
(Cambridge Univ. Cambridge, United Kingdom)
Pellegrino, S.
(Cambridge Univ. Cambridge, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: NASA. Johnson Space Center, The 29th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
95N27283
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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