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Vibration Testing of Electrical Cables to Quantify Loads at Tie-Down LocationsThe standard method for defining static equivalent structural load factors for components is based on Mile s equation. Unless test data is available, 5% critical damping is assumed for all components when calculating loads. Application of this method to electrical cable tie-down hardware often results in high loads, which often exceed the capability of typical tie-down options such as cable ties and P-clamps. Random vibration testing of electrical cables was used to better understand the factors that influence component loads: natural frequency, damping, and mass participation. An initial round of vibration testing successfully identified variables of interest, checked out the test fixture and instrumentation, and provided justification for removing some conservatism in the standard method. Additional testing is planned that will include a larger range of cable sizes for the most significant contributors to load as variables to further refine loads at cable tie-down points. Completed testing has provided justification to reduce loads at cable tie-downs by 45% with additional refinement based on measured cable natural frequencies.
Document ID
20140000633
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Dutson, Joseph D.
(Alliant Techsystems, Inc. Corrine, UT, United States)
Date Acquired
February 9, 2014
Publication Date
June 4, 2013
Subject Category
Mechanical Engineering
Report/Patent Number
M13-2654
Report Number: M13-2654
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.
Funding Number(s)
CONTRACT_GRANT: NNM07AA75C
Distribution Limits
Public
Copyright
Public Use Permitted.
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