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100   $a20130912j199909    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept /$fH. Kevin Rivers
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 1999.
215   $a1 online resource (13 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209560
300   $a"September 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 11).
517 3 $aCyclic cryogenic thermal-mechanical testing of an X-33 reusable launch vehicle liquid oxygen tank concept
606   $a7$aCyclic loads$2nasat
606   $aStorage tanks$2nasat
606   $aPropellant tanks$2nasat
606   $aLoad tests$2nasat
606   $aLoad testing machines$2nasat
606   $aFlight simulation$2nasat
615  7$a7$aCyclic loads.
615  7$aStorage tanks.
615  7$aPropellant tanks.
615  7$aLoad tests.
615  7$aLoad testing machines.
615  7$aFlight simulation.
700   $aRivers$b H. Kevin$01419508
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706133503321
996   $aCyclic cryogenic thermal-mechanical testing of an X-33$93534252
997   $aUNINA