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High-toughness graphite/epoxy composite material experimentThis experiment was designed to measure the effect of near-earth space exposure on three mechanical properties of specially toughened 5208/T300 graphite/epoxy composite materials. The properties measured are elastic modulus, strength, and fracture toughness. Six toughness specimens and nine tensile specimens were mounted on an external frame during the 5.8-year orbit of the Long Duration Exposure Facility (LDEF). Three identical sets of specimens were manufactured at the outset: the flight set, a zero-time non-flight set, and a total-time non-flight set.
Document ID
19930019074
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Felbeck, David K.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Publication Information
Publication: NASA. Langley Research Center, LDEF: 69 Months in Space. Part 3: Second Post-Retrieval Symposium
Subject Category
Composite Materials
Accession Number
93N28263
Funding Number(s)
CONTRACT_GRANT: NAS1-17008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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