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Graphite fluoride fibers and their applications in the space industryCharacterization and potential space applications of graphite fluoride fibers from commercially available graphitized carbon fibers are presented. Graphite fluoride fibers with fluorine to carbon ratios of 0.65 and 0.68 were found to have electrical resistivity values of 10(exp 4) and 10(exp 11) Ohms-cm, respectively, and thermal conductivity values of 24 and 5 W/m-K, respectively. At this fluorine content range, the fibers have tensile strength of 0.25 + or - 0.10 GPa (36 + or - 14 ksi), Young's modulus of 170 + or - 30 GPa (25 + or - 5 Msi). The coefficient of thermal expansion value of a sample with fluorine to carbon ratio of 0.61 was found to be 7 ppm/C. These properties change and approach the graphite value as the fluorine content approach 0. Electrically insulative graphite fluoride fiber is at least five times more thermally conductive than fiberglass. Therefore, it can be used as a heat sinking printed circuit board material for low temperature, long life power electronics in spacecraft. Also, partially fluorinated fiber with tailor-made physical properties to meet the requirements of certain engineering design can be produced. For example, a partially fluorinated fiber could have a predetermined CTE value in -1.5 to 7 ppm/C range and would be suitable for use in solar concentrators in solar dynamic power systems. It could also have a predetermined electrical resistivity value suitable for use as a low observable material. Experimental data indicate that slightly fluorinated graphite fibers are more durable in the atomic oxygen environment than pristine graphite. Therefore, fluorination of graphite used in the construction of spacecraft that would be exposed to the low Earth orbit atomic oxygen may protect defect sites in atomic oxygen protective coatings and therefore decrease the rate of degradation of graphite.
Document ID
19910001749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hung, Ching-Chen
(Cleveland State Univ. OH., United States)
Long, Martin
(NASA Lewis Research Center Cleveland, OH, United States)
Dever, Therese
(Cleveland State Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Subject Category
Chemistry And Materials (General)
Report/Patent Number
E-5679
NAS 1.15:103265
NASA-TM-103265
Report Number: E-5679
Report Number: NAS 1.15:103265
Report Number: NASA-TM-103265
Meeting Information
Meeting: AIChE Summer National Meeting
Location: San Diego, CA
Country: United States
Start Date: August 19, 1990
End Date: August 22, 1990
Accession Number
91N11062
Funding Number(s)
PROJECT: RTOP 505-41-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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