LEADER 01967nam  2200469   450 
001 9910705705003321
005 20170711091617.0
035   $a(CKB)5470000002453362
035   $a(OCoLC)993435119
035   $a(EXLCZ)995470000002453362
100   $a20170711j201703    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBuckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 2009 /$fMark W. Hilburger [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMarch 2017.
215   $a1 online resource (x, 91 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2017-219587
300   $a"March 2017."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 80).
517   $aBuckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02
606   $aBuckling$2nasat
606   $aCompression loads$2nasat
606   $aCylindrical shells$2nasat
606   $aLaunch vehicles$2nasat
606   $aAluminum alloys$2nasat
615  7$aBuckling.
615  7$aCompression loads.
615  7$aCylindrical shells.
615  7$aLaunch vehicles.
615  7$aAluminum alloys.
700   $aHilburger$b Mark W$g(Mark William),$01395062
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705705003321
996   $aBuckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 2009$93453051
997   $aUNINA