Evaluation Of Microcracking In Two Carbon-fiber/epoxy-matrix Composite Cryogenic Tanks

by Nasa Technical Reports Server (ntrs)

2021-01-13 20:34:20

Two graphite/epoxy cryogenic pressure vessels were evaluated for microcracking. The X-33 LH2 tank lobe skins were extensively examined for microcracks. Specimens were removed from the inner skin of the X-33 tank for tensile testing. The data obtained... Read more
Two graphite/epoxy cryogenic pressure vessels were evaluated for microcracking. The X-33 LH2 tank lobe skins were extensively examined for microcracks. Specimens were removed from the inner skin of the X-33 tank for tensile testing. The data obtained from these tests were used to model expected microcrack density as a function of stress. Additionally, the laminate used in the Marshall Space Flight Center (MSFC) Composite Conformal, Cryogenic, Common Bulkhead, Aerogel-Insulated Tank (CBAT) was evaluated. Testing was performed in an attempt to predict potential microcracking during testing of the CBAT. Less

Book Details

File size9.69 X 7.44 X 0.05 in
Print pages24
PublisherBiblioGov
Publication date August 2, 2013
LanguageEnglish
ISBN9781287274872

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