Report 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.
Structural Dynamics of Filament-Wound Booster Rockets
NASA Tech Briefs ; 11 , 9
1987-10-01
Miscellaneous
No indication
English
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