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Ares I-X USS Material TestingAn independent assessment was conducted to determine the critical initial flaw size (CIFS) for the flange-to-skin weld in the Ares I-X Upper Stage Simulator (USS). Material characterization tests were conducted to quantify the material behavior for use in the CIFS analyses. Fatigue crack growth rate, Charpy impact, and fracture tests were conducted on the parent and welded A516 Grade 70 steel. The crack growth rate tests confirmed that the material behaved in agreement with literature data and that a salt water environment would not significantly degrade the fatigue resistance. The Charpy impact tests confirmed that the fracture resistance of the material did not have a significant reduction for the expected operational temperatures of the vehicle.
Document ID
20080034824
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dawicke, David S.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Smith, Stephen W.
(NASA Langley Research Center 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-2008-215338
L-19517
NESC-RP-08-09/06-081-E
Report Number: NASA/TM-2008-215338
Report Number: L-19517
Report Number: NESC-RP-08-09/06-081-E
Funding Number(s)
WBS: WBS 510505.03.0701.11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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