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|Title: ||Issues related to large flight hardware acoustic qualification testing|
|Authors: ||Kolaini, Ali R.|
Perry, Douglas C.
Kern, Dennis L.
|Issue Date: ||29-Mar-2011 |
|Publisher: ||Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2011.|
|Citation: ||26th Aerospace Testing Seminar, El Segundo, California, March 29, 2011.|
|Abstract: ||The characteristics of acoustical testing volumes generated by reverberant chambers or a circle of loudspeakers with and without large flight hardware within the testing volume are significantly different. The parameters attributing to these differences are normally not accounted for through analysis or acoustic tests prior to the qualification testing without the test hardware present. In most cases the control microphones are kept at least 2-ft away from hardware surfaces, chamber walls, and speaker surfaces to minimize the impact of the hardware in controlling the sound field. However, the acoustic absorption and radiation of sound by hardware surfaces may significantly alter the sound pressure field controlled within the chamber/speaker volume to a given specification. These parameters often result in an acoustic field that may provide under/over testing scenarios for flight hardware. In this paper the acoustic absorption by hardware surfaces will be discussed in some detail. A simple model is provided to account for some of the observations made from Mars Science Laboratory spacecraft that
recently underwent acoustic qualification tests in a reverberant chamber.|
|Appears in Collections:||JPL TRS 1992+|
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