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High-toughness graphite/epoxy composite material experimentThis experiment was designed to measure the effect of near 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 time of the Long Duration Exposure Facility (LDEF) mission. 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. To date, two toughness specimens and three strength and modulus specimens have been tested from each of the three groups.
Document ID
19920015598
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
January 1, 1992
Publication Information
Publication: NASA. Langley Research Center, LDEF: 69 Months in Space. First Post-Retrieval Symposium, Part 2
Subject Category
Composite Materials
Accession Number
92N24841
Funding Number(s)
CONTRACT_GRANT: NAS1-17008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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