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Effects of experimentally measured pressure oscillations on the vibration of a solid rocket motorResults are presented of firing a Nike rocket against a backstop for the purpose of obtaining pressure fluctuations in the rocket case and determining their relationship to structural vibrations of the case. Special care was required to obtain these pressure fluctuations because of the much higher static pressure generated in the rocket. Very small pressure fluctuations within the rocket case can cause significant vibration levels. A previously observed high frequency was shown to decrease with time before completely disappearing at about 1 second of burning time. The vibration of the case itself is probably related to the longitudinal structural modes at frequencies below 500 Hz and is dependent on local structural conditions at frequencies above this value.
Document ID
19730002206
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Schoenster, J. A.
(NASA Langley Research Center Hampton, VA, United States)
Pierce, H. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-6931
L-8417
Report Number: NASA-TN-D-6931
Report Number: L-8417
Accession Number
73N10933
Funding Number(s)
PROJECT: RTOP 114-08-13-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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