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EVA assembly and release of highly loaded boltsThe modification of a multi-jackbolt mechanism, Superbolt(TM), for on-orbit release of highly loaded bolts is described. Preload and release test data demonstrate that modification of a commercial product produced a solution for the deployment of the Space Station Remote Manipulator System (SSRMS) that was less expensive, faster, and lighter than other alternatives. Using the Superbolt design, virtually unlimited bolt loads can be applied or released with a standard wrench.
Document ID
19960025617
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Olmstead, Jim (Spar Aerospace Ltd. Brampton, Ontario Canada)
Barker, Paul (Spar Aerospace Ltd. Brampton, Ontario Canada)
Date Acquired
August 17, 2013
Publication Date
May 1, 1996
Publication Information
Publication: 30th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
96N27623
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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