LEADER 01873nam  2200493   450 
001 9910705842203321
005 20170802104716.0
035   $a(CKB)5470000002453996
035   $a(OCoLC)998818765
035   $a(EXLCZ)995470000002453996
100   $a20170802j199807    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFeasibility assessment of thermal barrier seals for extreme transient temperatures /$fBruce M. Steinetz, Patrick H. Dunlap, Jr
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJuly 1998.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208484
300   $a"July 1998."
300   $a"Prepared for the 34th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 12-15, 1998."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-98-3288."
320   $aIncludes bibliographical references (pages 8-9).
606   $aFeasibility analysis$2nasat
606   $aThermal resistance$2nasat
606   $aSealing$2nasat
606   $aHigh temperature gases$2nasat
606   $aO ring seals$2nasat
615  7$aFeasibility analysis.
615  7$aThermal resistance.
615  7$aSealing.
615  7$aHigh temperature gases.
615  7$aO ring seals.
700   $aSteinetz$b Bruce M.$01393619
702   $aDunlap$b Patrick H.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705842203321
996   $aFeasibility assessment of thermal barrier seals for extreme transient temperatures$93536427
997   $aUNINA