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035   $a(CKB)5470000002452743
035   $a(OCoLC)703646063
035   $a(EXLCZ)995470000002452743
100   $a20110225j199711    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe impact response of carbon/epoxy laminates /$fA.T. Nettles and A.J. Hodge
210  1$aMarshall Space Flight Center, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dNovember 1997.
215   $a1 online resource (viii, 165 pages) $cillustrations
225 1 $aNASA/TM ;$v97-206317
300   $a"November 1997."
300   $a"Performing organization: George C. Marshall Space Flight Center"-- Report documentation page.
320   $aIncludes bibliographical references (pages 155-165).
606   $aEpoxy matrix composites$2nasat
606   $aLaminates$2nasat
606   $aImpact tests$2nasat
606   $aDynamic tests$2nasat
608   $aTechnical Memorandum.
610   $aImpact Phenomena
615  7$aEpoxy matrix composites.
615  7$aLaminates.
615  7$aImpact tests.
615  7$aDynamic tests.
700   $aNettles$b A. T$g(Alan T.),$01389578
702   $aHodge$b A. J.
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bSSM
801  1$bSSM
801  2$bGPO
906   $aBOOK
912   $a9910705766303321
996   $aThe impact response of carbon$93533195
997   $aUNINA