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Lock-up failure of a four-bar linkage deployment mechanismA successful failure investigation of a four-bar linkage deployment mechanism has been performed. Possible failure causes such as the mismatch of material coefficient of thermal expansion (CTE), excessive hinge friction, limit switch interference, and thermal gradient induced resistive preload were investigated and are discussed. The final conclusions and corrective actions taken are described. Finally, valuable lessons learned during the investigation are discussed.
Document ID
19940025143
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zinn, Michael
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Publication Information
Publication: NASA. Ames Research Center, The 27th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
94N29646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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