LEADER 01935nam  2200541 a 450 
001 9910699506003321
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035   $a(CKB)5470000002403871
035   $a(OCoLC)681742049
035   $a(EXLCZ)995470000002403871
100   $a20101117d2009      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA comparison of the capability of sensitivity level 3 and sensitivity level 4 fluorescent penetrants to detect fatigue cracks in aluminum$b[electronic resource] /$fBradford H. Parker
210  1$aGreenbelt, Md. :$cNational Aeronautics and Space Administration, Goddard Space Flight Center,$d[2009]
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA/TM ;$v2009-215850
300   $aTitle from title screen (viewed on Oct. 22, 2010).
300   $a"December 2009."
320   $aIncludes bibliographical references (page 16).
410  0$aNASA technical memorandum ;$v2009-215850.
606   $aInspection$2nasat
606   $aQuality control$2nasat
606   $aNondestructive tests$2nasat
606   $aCracks$2nasat
606   $aPenetrants$2nasat
606   $aProbability theory$2nasat
606   $aMetal fatigue$2nasat
606   $aDetection$2nasat
615  7$aInspection.
615  7$aQuality control.
615  7$aNondestructive tests.
615  7$aCracks.
615  7$aPenetrants.
615  7$aProbability theory.
615  7$aMetal fatigue.
615  7$aDetection.
700   $aParker$b Bradford H$01395870
712 02$aGoddard Space Flight Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699506003321
996   $aA comparison of the capability of sensitivity level 3 and sensitivity level 4 fluorescent penetrants to detect fatigue cracks in aluminum$93484231
997   $aUNINA