LEADER 01633oam 2200481I 450 001 9910705766303321 005 20170619132241.0 035 $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