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035   $a(CKB)5470000002469459
035   $a(OCoLC)973491877
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100   $a20170223j199610    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of metallic thermal protection systems for the reusable launch vehicle /$fMax L. Blosser
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1996.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110296
300   $a"October 1996."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
300   $a"Presented at the Space Technology and Applications Albuquerque, New Mexico, on January 26-30, 1997"--Report documentation page.
320   $aIncludes bibliographical references (pages 20-21).
606   $aThermal protection$2nasat
606   $aStructural analysis$2nasat
606   $aReusable launch vehicles$2nasat
606   $aHypervelocity impact$2nasat
606   $aHeat resistant alloys$2nasat
615  7$aThermal protection.
615  7$aStructural analysis.
615  7$aReusable launch vehicles.
615  7$aHypervelocity impact.
615  7$aHeat resistant alloys.
700   $aBlosser$b Max L.$01400718
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707911403321
996   $aDevelopment of metallic thermal protection systems for the reusable launch vehicle$93486332
997   $aUNINA