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External Tank (ET) Bipod Fitting Bolted Attachment Locking Insert PerformanceFollowing STS-107, the External Tank (ET) Project implemented corrective actions and configuration changes at the ET bipod fitting. Among the corrective actions, the existing bolt lock wire which provided resistance to potential bolt rotation was removed. The lock wire removal was because of concerns with creating voids during foam application and potential for lock wire to become debris. The bolts had been previously lubricated to facilitate assembly but, because of elimination of the lock wire, the ET Project wanted to enable the locking feature of the insert. Thus, the lubrication was removed from bolt threads and instead applied to the washer under the bolt head. Lubrication is necessary to maximize joint pre-load while remaining within the bolt torque specification. The locking feature is implemented by thread crimping in at four places in the insert. As the bolt is torqued into the insert the bolt threads its way past the crimped parts of the insert. This provides the locking of the bolt, as torque is required to loosen the joint after clamping.
Document ID
20080007518
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Larsen, Curtis E.
(NASA Johnson Space Center Houston, TX, United States)
Wilson, Tim R.
(NASA Langley Research Center Hampton, VA, United States)
Elliott, Kenny B.
(NASA Langley Research Center Hampton, VA, United States)
Raju, Ivatury S.
(NASA Langley Research Center Hampton, VA, United States)
McManamen, John
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2008-215099
NESC-RP-06-53/06-032-E
L-19439
Report Number: NASA/TM-2008-215099
Report Number: NESC-RP-06-53/06-032-E
Report Number: L-19439
Funding Number(s)
WBS: WBS 510505.01.07.01.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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