LEADER 01595nam  2200469 a 450 
001 9910702004903321
005 20120912090752.0
035   $a(CKB)5470000002424084
035   $a(OCoLC)809789670
035   $a(EXLCZ)995470000002424084
100   $a20120912d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComposite stress rupture$b[electronic resource] $ea new reliability model based on strength decay /$fJames R. Reeder
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (24 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217566
300   $aTitle from title screen (viewed on Sept. 12, 2012).
300   $a"April 2012."
320   $aIncludes bibliographical references (page 24).
517   $aComposite stress rupture 
606   $aComposite wrapping$2nasat
606   $aReliability analysis$2nasat
606   $aPressure vessels$2nasat
606   $aComposite structures$2nasat
606   $aCreep rupture strength$2nasat
615  7$aComposite wrapping.
615  7$aReliability analysis.
615  7$aPressure vessels.
615  7$aComposite structures.
615  7$aCreep rupture strength.
700   $aReeder$b James R$01405865
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702004903321
996   $aComposite stress rupture$93483220
997   $aUNINA