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Finite element model of SCOLE laboratory configurationThe Spacecraft Control Laboratory Experiment (SCOLE) is defined by element properties: material constants; mast, reflector, rigid links as beam elements; cable as bar element; and space shuttle as very stiff beam. Two boundary conditions are modeled: suspended (6 degrees of freedom for all joints except the top of the cable) and cantilevered cables (shuttle platform fixed in all degrees of freedon). Calculations include stiffness and mass matrices, initial stresses, static displacements and reactions, and eigensolutions.
Document ID
19870008395
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, Beth
(NASA Langley Research Center Hampton, VA, United States)
Williams, Jeffrey P.
(NASA Langley Research Center Hampton, VA, United States)
Sparks, Dean
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: Proceedings of the 3rd Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17828
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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