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Conservative torques and moments of inertia involved in the design of a laboratory model solar array with variable paddle-arm orientationDesign of electromechanical satellite solar paddle orientation model including conservative torques and inertia of rotation axis
Document ID
19660022790
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mc Carron, S. G. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1963
Subject Category
Auxiliary Systems
Accession Number
66N32080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ELECTROMECHANICAL DEVICE
SOLAR CELL
ROTATING SHAFT
SATELLITE INSTRUMENTATION
INSTRUMENT ORIENTATION
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IDRelationTitle19660022754Collected WorksPublications of Goddard Space Flight Center, 1963. Volume II - Space technology19660022754Collected WorksPublications of Goddard Space Flight Center, 1963. Volume II - Space technologyN66-32044 18-31Collected Works
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