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Analytical study of lightweight acoustic shrouds for shuttle experiments and payloadsResults are presented of acoustic tests performed on an STS payload shroud simulator to determine the effects of a helium filled liner on the noise reduction characteristics. The basic test program included the following configurations: (1) bare shroud (baseline configuration); (2) shroud with empty liner; (3) shroud with liner filled with air; and (4) shroud with liner filled with helium. The results indicate negligible effects from the helium. Configurations for liner filled with air, and liner filled with helium were also tested. The data from these configurations indicate increased noise reduction from the use of helium.
Document ID
19770005170
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baratono, J.
(Martin Marietta Corp. Denver, CO, United States)
Rader, P.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1976
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-150116
MCR-76-465
Report Number: NASA-CR-150116
Report Number: MCR-76-465
Accession Number
77N12113
Funding Number(s)
CONTRACT_GRANT: NAS8-31912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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