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Carbon/Phenolic Nanocomposites as Advanced Thermal Protection Material in Aerospace Applications
Author(s) -
Jitendra Tate,
S.D. Gaikwad,
Nikoleta Theodoropoulou,
E. Trevino,
Joseph H. Koo
Publication year - 2013
Publication title -
journal of composites
Language(s) - English
Resource type - Journals
eISSN - 2356-7252
pISSN - 2314-5978
DOI - 10.1155/2013/403656
Subject(s) - materials science , composite material , nanocomposite , carbon nanotube , composite number , dispersion (optics) , carbon black , carbon fibers , mixing (physics) , epoxy , natural rubber , physics , quantum mechanics , optics
Ablative nanocomposites were prepared by incorporating multiwall carbon nanotubes (MWCNT) into phenolic resin and then impregnating them into rayon-based carbon fabric. MWCNT were blended into phenolic resin at 0.5, 1, and 2 wt% loadings using a combination of sonication and high shear mixing to insure uniform dispersion of MWCNT. The composite test specimens were tested by using an oxyacetylene test bed (OTB) applying a heat flux of 1000 W/cm2 for duration of 45 seconds. Composite specimens with 2 wt% MWCNT showed reduction in mass loss, recession in length, and in situ temperatures compared to control composites

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