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Ares I-X Upper Stage Simulator Structural Analyses Supporting the NESC Critical Initial Flaw Size AssessmentThe structural analyses described in the present report were performed in support of the NASA Engineering and Safety Center (NESC) Critical Initial Flaw Size (CIFS) assessment for the ARES I-X Upper Stage Simulator (USS) common shell segment. The structural analysis effort for the NESC assessment had three thrusts: shell buckling analyses, detailed stress analyses of the single-bolt joint test; and stress analyses of two-segment 10 degree-wedge models for the peak axial tensile running load. Elasto-plastic, large-deformation simulations were performed. Stress analysis results indicated that the stress levels were well below the material yield stress for the bounding axial tensile design load. This report also summarizes the analyses and results from parametric studies on modeling the shell-to-gusset weld, flange-surface mismatch, bolt preload, and washer-bearing-surface modeling. These analyses models were used to generate the stress levels specified for the fatigue crack growth assessment using the design load with a factor of safety.
Document ID
20080034821
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Knight, Norman F., Jr.
(General Dynamics Advanced Information Systems Chantilly, VA, United States)
Phillips, Dawn R.
(Lockheed Martin Mission Services Co. Hampton, VA, United States)
Raju, Ivatury S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
August 1, 2008
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2008-215336
NESC-RP-08-09/06-081-E
L-19514
Report Number: NASA/TM-2008-215336
Report Number: NESC-RP-08-09/06-081-E
Report Number: L-19514
Funding Number(s)
WBS: WBS 510505.03.0701.11
Distribution Limits
Public
Copyright
Public Use Permitted.
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