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Structural design/margin assessmentDetermining structural design inputs and the structural margins following design completion is one of the major activities in space exploration. The end result is a statement of these margins as stability, safety factors on ultimate and yield stresses, fracture limits (fracture control), fatigue lifetime, reuse criteria, operational criteria and procedures, stability factors, deflections, clearance, handling criteria, etc. The process is normally called a load cycle and is time consuming, very complex, and involves much more than structures. The key to successful structural design is the proper implementation of the process. It depends on many factors: leadership and management of the process, adequate analysis and testing tools, data basing, communications, people skills, and training. This process and the various factors involved are discussed.
Document ID
19940008358
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ryan, R. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TP-3410
NAS 1.60:3410
M-730
Report Number: NASA-TP-3410
Report Number: NAS 1.60:3410
Report Number: M-730
Accession Number
94N12831
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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