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Self-shadowing of orbiting trussesThe approach used to assess shadowing reductions on the heating of orbiting trusses involves determining the heating rates with slender member shadowing effects included and then obtaining the thermal response of the shadowed member. Steps taken to identify shadowers, find locations where shadowing occurs and calculate shadow intensity are listed. The finite element thermal structural analysis of cable stiffened space structure is delineated and the exact solution of the caternary problem is given. Typical cable surface heating rates are plotted. The structural analysis includes large deformation (nonlinear), thermal effect, and the pretension effect. Displacements and stresses are computed at different orbital positions for an orbit.
Document ID
19840008497
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mahaney, J.
(Old Dominion Univ. Norfolk, VA, United States)
Thornton, E. A.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1983
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-173215
NAS 1.26:173215
Report Number: NASA-CR-173215
Report Number: NAS 1.26:173215
Accession Number
84N16565
Funding Number(s)
CONTRACT_GRANT: NAG1-257
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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