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Pre-Test Analysis Predictions for the Shell Buckling Knockdown Factor Checkout Tests - TA01 and TA02This report summarizes the pre-test analysis predictions for the SBKF-P2-CYL-TA01 and SBKF-P2-CYL-TA02 shell buckling tests conducted at the Marshall Space Flight Center (MSFC) in support of the Shell Buckling Knockdown Factor (SBKF) Project, NASA Engineering and Safety Center (NESC) Assessment. The test article (TA) is an 8-foot-diameter aluminum-lithium (Al-Li) orthogrid cylindrical shell with similar design features as that of the proposed Ares-I and Ares-V barrel structures. In support of the testing effort, detailed structural analyses were conducted and the results were used to monitor the behavior of the TA during the testing. A summary of predicted results for each of the five load sequences is presented herein.
Document ID
20110004286
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Thornburgh, Robert P.
(Army Research Lab. Hampton, VA, United States)
Hilburger, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Space Transportation And Safety
Report/Patent Number
L-19958
NF1676L-11908
NASA/TM-2011-216875
ARL-TR-5123
Report Number: L-19958
Report Number: NF1676L-11908
Report Number: NASA/TM-2011-216875
Report Number: ARL-TR-5123
Funding Number(s)
WBS: WBS 869021.04.07.01.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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