LEADER 01733nam  2200493I  450 
001 9910704629203321
005 20130705144259.0
035   $a(CKB)5470000002443425
035   $a(OCoLC)851803234
035   $a(EXLCZ)995470000002443425
100   $a20130705d2013      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNormalization of impact energy by laminate thickness for compression after impact testing /$fA.T. Nettles and S.M. Hromisin
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d2013.
215   $a1 online resource (ix, 37 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2013-217481
300   $aTitle from title screen (viewed on July 5, 2013).
300   $a"April 2013."
320   $aIncludes bibliographical references (pages 35-37).
606   $aLaminates$2nasat
606   $aThickness$2nasat
606   $aImpact strength$2nasat
606   $aCompression loads$2nasat
606   $aMechanical properties$2nasat
606   $aImpact tolerances$2nasat
615  7$aLaminates.
615  7$aThickness.
615  7$aImpact strength.
615  7$aCompression loads.
615  7$aMechanical properties.
615  7$aImpact tolerances.
700   $aNettles$b A. T$g(Alan T.),$01389578
702   $aHromisin$b S. M.
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704629203321
996   $aNormalization of impact energy by laminate thickness for compression after impact testing$93491715
997   $aUNINA