LEADER 01797nam  2200529I  450 
001 9910707912803321
005 20170223085947.0
035   $a(CKB)5470000002469445
035   $a(OCoLC)973480417
035   $a(EXLCZ)995470000002469445
100   $a20170223j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aProperties of two carbon composite materials using LTM25 epoxy resin /$fJuan R. Cruz, C.H. Shah and A.S. Postyn
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1996.
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110286
300   $a"November 1996."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (page 9).
606   $aEpoxy resins$2nasat
606   $aCarbon fibers$2nasat
606   $aCuring$2nasat
606   $aComposite structures$2nasat
606   $aEnvironmental tests$2nasat
606   $aEpoxy matrix composites$2nasat
606   $aPrepregs$2nasat
615  7$aEpoxy resins.
615  7$aCarbon fibers.
615  7$aCuring.
615  7$aComposite structures.
615  7$aEnvironmental tests.
615  7$aEpoxy matrix composites.
615  7$aPrepregs.
700   $aCross$b John R.$0128648
702   $aShah$b C. H.
702   $aPostyn$b A. S.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707912803321
996   $aProperties of two carbon composite materials using LTM25 epoxy resin$93544803
997   $aUNINA