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Preloaded Joint Analysis Methodology for Space Flight SystemsThis report contains a compilation of some of the most basic equations governing simple preloaded joint systems and discusses the more common modes of failure associated with such hardware. It is intended to provide the mechanical designer with the tools necessary for designing a basic bolted joint. Although the information presented is intended to aid in the engineering of space flight structures, the fundamentals are equally applicable to other forms of mechanical design.
Document ID
19960012183
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Jeffrey A Chambers
(Glenn Research Center Cleveland, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1995
Subject Category
Mechanical Engineering
Report/Patent Number
NIPS-96-08130
NASA-TM-106943
NAS 1.15:106943
E-9672
Accession Number
96N18420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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