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An experimental investigation of noise attenuating techniques for space-shuttle canistersA model of the space shuttle thermal canister was acoustically tested to determine the amount of noise attenuation which could be derived using a simple, single-wall canister construction having rectangular shape. Acoustic testing was performed on the basic canister and with noise-attenuating design modifications. The basic canister experienced noise amplifications at 56 and 80 Hz, which are attributed to the fundamental canister acoustic mode and local panel structural resonances, respectively. The standing wave response at 56 Hz was effectively suppressed by the incorporation of a cardboard baffle midway between the canister end-caps (an additional overall noise reduction of 4 dB). The canister was next tested with 14%, 22.5% and 31% sound absorptive coverages on the interior walls. The coverage was effective between 400-3000 Hz; the maximum benefit (9 dB) occurring at 1600 Hz. Viscoelastic damping strips bonded to the canister exterior provided an additional 4 to 5 dB attenuation over much of the frequency range and has an overall reduction of about 10 dB as compared to 4.4 dB without damping. A significant reduction of the resonant effect at 80 Hz was noted.
Document ID
19830022530
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mirandy, L.
(General Electric Co. Greenbelt, MD, United States)
On, F. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Scott, J.
(NASA Goddard Space Flight Center)
Date Acquired
August 11, 2013
Publication Date
September 1, 1980
Publication Information
Publication: Shock and Vibration Inform. Center The Shock and Vibration Bull., No. 50, Part 4
Subject Category
Space Transportation
Accession Number
83N30801
Funding Number(s)
CONTRACT_GRANT: NAS5-23412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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