| Record ID | bcl_marc/bcl_open.03.mrc:170297909:1619 |
| Source | bcl_marc |
| Download Link | /show-records/bcl_marc/bcl_open.03.mrc:170297909:1619?format=raw |
LEADER: 01619nam 22003977a 4500
003 OCoLC
004 GPM1655
005 20000524102000.0
008 960118s1994 dcu b f000 0 eng d
035 $a(OCoLC)ocm34051876
035 9 $aGPM1655
037 $aN 95-31419$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aBXMX
074 $a0830-D (MF)
086 0 $aNAS 1.15:110625
100 1 $aSerdinak, Thomas E.
245 10 $aPost-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites$h[microform] /$cby Thomas E. Serdinak.
246 2 $aPost impact fatigue of cross plied, through the thickness reinforced carbon/expoxy composites
260 $a[Washington, DC :$bNational Aeronautics and Space Administration ;$aSpringfield, Va. :$bNational Technical Information Service, distributor,$c1995]
300 $a1 v.
490 1 $aNASA-TM ;$v110625
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 96-0033-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1995]$e2 microfiches.
650 7 $aEpoxy matrix composites.$2nasat
650 7 $aFatigue (Materials)$2nasat
650 7 $aFatigue tests.$2nasat
650 7 $aImpact damage.$2nasat
650 7 $aReinforcing fibers.$2nasat
650 7 $aStress-strain relationships.$2nasat
650 7 $aWoven composites.$2nasat
710 1 $aUnited States.$bNational Aeronautics and Space Administration.
830 0 $aNASA technical memorandum$v110625..
852 30 $aMChB$bGOV$cFICHE$hNAS 1.15:110625$91
948 $aLTI 08/08/2000