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Structural Dynamics of Filament-Wound Booster RocketsReport summarizes program of measurements and calculations of vibrations in filament-wound composite models of Space Shuttle solid-rocket boosters. Vibrational behavior predicted by finite-element computer model of structural dynamics correlates well with data from tests on full- and quarter-scale models. Computer model developed with NASTRAN general-purpose structural-analysis computer code.
Document ID
19870000489
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bugg, F. M. (NASA Marshall Space Flight Center, Huntsville, Ala.)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-28155
Accession Number
87B10489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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