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Acoustic Analysis and Design of the E-STA MSA SimulatorThe Orion European Service Module Structural Test Article (E-STA) Acoustic Test was completed in May 2016 to verify that the European Service Module (ESM) can withstand qualification acoustic environments. The test article required an aft closeout to simulate the Multi-Purpose Crew Vehicle (MPCV) Stage Adapter (MSA) cavity, however, the flight MSA design was too cost-prohibitive to build. NASA Glenn Research Center (GRC) had 6 months to design an MSA Simulator that could recreate the qualification prediction MSA cavity sound pressure level to within a reasonable tolerance. This paper summarizes the design and analysis process to arrive at a design for the MSA Simulator, and then compares its performance to the final prediction models created prior to test.
Document ID
20160014882
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Bittinger, Samantha A.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
December 29, 2016
Publication Date
December 1, 2016
Subject Category
Spacecraft Design, Testing And Performance
Acoustics
Report/Patent Number
E-19322
GRC-E-DAA-TN37647
NASA/TM-2016-219434
Funding Number(s)
WBS: WBS 747797.02.04.30.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
acoustics
test
orion
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