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035   $a(OCoLC)703645444
035   $a(EXLCZ)995470000002462127
100   $a20110225j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA new aging treatment for improving cryogenic toughness of the main structural alloy of the super lightweight tank /$fP.S. Chen, W.P. Stanton
210  1$aMSFC, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dNovember 1996.
215   $a1 online resource (vii, 10 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v108524
300   $aTitle from title screen (viewed May 6, 2016).
300   $a"November 1996."
300   $a"Performing organization: George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama"--Report documentation page.
320   $aIncludes bibliographical references (page 4).
606   $aAging (materials)$2nasat
606   $aAluminum alloys$2nasat
606   $aCryogenic temperature$2nasat
606   $aFracture strength$2nasat
606   $aPrecipitation hardening$2nasat
608   $aTechnical Memorandum.
615  7$aAging (materials)
615  7$aAluminum alloys.
615  7$aCryogenic temperature.
615  7$aFracture strength.
615  7$aPrecipitation hardening.
700   $aChen$b P. S.$01414886
702   $aStanton$b W. P.
712 02$aGeorge C. Marshall Space Flight Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bSSM
801  1$bSSM
801  2$bGPO
906   $aBOOK
912   $a9910707137203321
996   $aA new aging treatment for improving cryogenic toughness of the main structural alloy of the super lightweight tank$93515378
997   $aUNINA