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Resolution of Forces and Strain Measurements from an Acoustic Ground TestThe Conservatism in Typical Vibration Tests was Demonstrated: Vibration test at component level produced conservative force reactions by approximately a factor of 4 (approx.12 dB) as compared to the integrated acoustic test in 2 out of 3 axes. Reaction Forces Estimated at the Base of Equipment Using a Finite Element Based Method were Validated: FEM based estimate of interface forces may be adequate to guide development of vibration test criteria with less conservatism. Element Forces Estimated in Secondary Structure Struts were Validated: Finite element approach provided best estimate of axial strut forces in frequency range below 200 Hz where a rigid lumped mass assumption for the entire electronics box was valid. Models with enough fidelity to represent diminishing apparent mass of equipment are better suited for estimating force reactions across the frequency range. Forward Work: Demonstrate the reduction in conservatism provided by; Current force limited approach and an FEM guided approach. Validate proposed CMS approach to estimate coupled response from uncoupled system characteristics for vibroacoustics.
Document ID
20140000635
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Smith, Andrew M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
LaVerde, Bruce T.
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Hunt, Ronald
(BRC, Inc. Huntsville, AL)
Waldon, James M.
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
February 9, 2014
Publication Date
June 4, 2013
Subject Category
Acoustics
Report/Patent Number
M13-2669
Meeting Information
Meeting: Spacecraft and Launch Vehicle Dynamic Environments Workshop
Location: El Segundo, CA
Country: United States
Start Date: June 4, 2013
End Date: June 6, 2013
Sponsors: Aerospace Corp.
Distribution Limits
Public
Copyright
Public Use Permitted.
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