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Space environmental effects on graphite-epoxy compressive properties and epoxy tensile propertiesThis study characterizes the effects of electron radiation and temperature on a graphite-epoxy composite material. Compressive properties of the T300/934 material system were obtained at -250 F (-157 C), room temperature, and 250 F (121 C). Tensile specimens of the Fiberite 934 epoxy resin were fabricated and tested at room temperature and 250 F (121 C). Testing was conducted in the baseline (nonirradiated) and irradiated conditions. The radiation exposure was designed to simulate 30 year, worst-case exposure in geosynchronous Earth orbit. Mechanical properties tended to degrade at elevated temperature and improve at cryogenic temperature. Irradiation generally degraded properties at all temperatures.
Document ID
19870016722
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fox, Derek J.
(NASA Langley Research Center Hampton, VA, United States)
Sykes, George F., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Herakovich, Carl T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg., United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1987
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-89297
VPI-E-87-13
CCMS-87-11
NAS 1.15:89297
Report Number: NASA-TM-89297
Report Number: VPI-E-87-13
Report Number: CCMS-87-11
Report Number: NAS 1.15:89297
Accession Number
87N26155
Funding Number(s)
CONTRACT_GRANT: NAG1-343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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