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Test-Analysis Correlation of the Single Stringer Bending Tests for the Space Shuttle ET-137 Intertank Stringer Crack Investigation

机译:航天飞机ET-137内箱纵梁裂纹研究的单纵梁弯曲试验的测试分析相关性

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Following the scrub of the November 5, 2010 launch attempt of Space Shuttle mission STS-133, cracks were found in the stringers on the Intertank of the External Tank, ET-137. A large investigation was conducted to determine the root cause of the cracks, establish a repair for the stringers, and provide data for the flight readiness assessment of the repaired tank. As part of the investigation, static load tests of individual stringer-skin sections and corresponding finite element analyses were performed. The details of these finite element analyses and the test-analysis correlation for these single stringer bending tests are presented. Comparisons and contrasts between the analyses and test results for two specific stringers are made and used to discuss challenges related to modeling for quickly-developed test programs; correlation of the finite element models to the test data was not trivial and is discussed. The analyses and test results are also discussed as they related to the development of the flight-worthiness rationale for ET-137 and the tanks for the remaining Shuttle missions. Lessons learned are identified.
机译:在2010年11月5日航天飞机任务STS-133发射尝试被擦洗之后,在外部坦克ET-137的Intertank的纵梁上发现了裂缝。进行了大规模调查,以确定裂纹的根本原因,对桁条进行了维修,并为维修后的油箱的飞行准备状态评估提供了数据。作为研究的一部分,对单个纵梁截面进行了静载荷测试,并进行了相应的有限元分析。给出了这些有限元分析的细节以及这些单纵梁弯曲试验的试验分析相关性。对两个特定纵梁的分析和测试结果进行了比较和对比,并用于讨论与快速开发的测试程序的建模有关的挑战;有限元模型与测试数据之间的相关性并非微不足道,并进行了讨论。还讨论了分析和测试结果,因为它们与ET-137的飞行适航性原理以及其余航天飞机任务的坦克的发展有关。确定吸取的教训。

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