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Convected transient analysis for large space structures maneuver and deploymentConvected-transient analysis techniques in the finite-element method are used to investigate the deployment and maneuver of large spacecraft structures with multiple-member flexible trusses and frames. Numerical results are presented for several sample problems.
Document ID
19840048965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Housner, J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 84-1023
Report Number: AIAA PAPER 84-1023
Accession Number
84A31752
Distribution Limits
Public
Copyright
Other

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