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035   $a(OCoLC)688502536
035   $a(EXLCZ)995470000002385247
100   $a20101201d2005      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue crack growth rate of Inconel 718 sheet at cryogenic temperatures$b[electronic resource] $eNASA Engineering and Safety Center, Materials Super Problem Resolution Team activity report /$fDouglas Wells, Jonathan Wright and Keith Hastings
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2005]
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA/TM- ;$v2005-213948
300   $aTitle from title screen (viewed on Dec. 1, 2010).
300   $a"December 2005."
320   $aIncludes bibliographical references (page 7)
410  0$aNASA technical memorandum ;$v213948.
517   $aFatigue crack growth rate of Inconel 718 sheet at cryogenic temperatures 
606   $aLiquid hydrogen$2nasat
606   $aInconel (trademark)$2nasat
606   $aCrack propagation$2nasat
615  7$aLiquid hydrogen.
615  7$aInconel (trademark)
615  7$aCrack propagation.
700   $aWells$b Douglas$01413092
701   $aWright$b Jonathan$0691843
701   $aHastings$b Keith$01413093
712 02$aLangley Research Center.
712 02$aNASA Engineering and Safety Center.$bMaterials Super Problem Resolution Team.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697166403321
996   $aFatigue crack growth rate of Inconel 718 sheet at cryogenic temperatures$93508649
997   $aUNINA