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Bi-Axial Load Testing of a Woven-Webbing Inflatable Space Habitat Restraint Layer ComponentThis report discusses testing of a bi-axial woven panel consisting of high-strength webbings that represent a portion of the structural restraint layer of an inflatable space structure. Inflatable softgoods vessels are being researched for human space missions as possible habitats, airlocks and tunnel elements. Understanding the complex behavior of the softgoods restraint layer and maturing finite element analysis capabilities to model these structures is critical to their successful implementation. The primary goal of this research is to study the load-up and load distribution in a weave of webbings, before and after the loss of tension in one of the webbings. In addition, a key objective is to evaluate the ability to convert strains measured via photogrammetry using digital image correlation to loads in the weave. The report gives an introduction and objectives for the test program and a description of the test fixture, setup and procedure. This is followed by a section focusing on the test data and associated discussion. To streamline presentation of the data, one focus case is detailed in the main text. (Comprehensive data set can be found in Appendix A for the three remaining test cases.) In addition to the load and time histories for one case, summary charts and tables that incorporate data from all four test cases are provided. The concluding remarks include major findings, lessons learned and recommendations for future work. Appendix B provides complementary full-field strain results when considering the existing woven webbing data as a fabric. These types of results could inform models intended for global representation. Appendix C contains a description from a series of exploratory instrumented hammer tap tests and results on the weave. These tests describe an area of research for the biaxial test fixture beyond the current testing studying the propagation and detection of vibrations in a tensioned weave that has applications in impact and damage detection.
Document ID
20200002948
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Karen H Lyle
(Langley Research Center Hampton, Virginia, United States)
Thomas C Jones
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 22, 2020
Publication Date
March 1, 2020
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-36007
NASA/TM-2020-220575
Report Number: NF1676L-36007
Funding Number(s)
WBS: 089407.09.23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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