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100   $a20140102j199207    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials /$fCynthia L. Lach
210  1$aWashington, DC :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dJuly 1992.
215   $a1 online resource (approximately 18 pages) $cillustrations
225 1 $aNASA/TP ;$v3226
300   $a"July 1992."
320   $aIncludes bibliographical references (page 11).
606   $aResilience$2nasat
606   $aElastomers$2nasat
606   $aBooster rocket engines$2nasat
606   $aSealing (Technology)$xMaterials$xTesting
606   $aElastomers$xTesting
606   $aRockets (Aeronautics)$xMaterials$xTesting
606   $aElastomers$xTesting$2fast
615  7$aResilience.
615  7$aElastomers.
615  7$aBooster rocket engines.
615  0$aSealing (Technology)$xMaterials$xTesting.
615  0$aElastomers$xTesting.
615  0$aRockets (Aeronautics)$xMaterials$xTesting.
615  7$aElastomers$xTesting.
700   $aLach$b Cynthia L.$01417361
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910717009203321
996   $aEffect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials$93525468
997   $aUNINA