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101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAlkali metal backup cooling for Stirling systems, experimental results /$fCarl Schwendeman [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2013.
215   $a1 online resource (15 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-216591
300   $aTitle from title screen (viewed on March 25, 2015).
300   $a"October 2013."
300   $a"Prepared for the Nuclear and Emerging Technologies for Space (NETS-2013) sponsored by the Aerospace Nuclear Society and Aerojet, Albuquerque, New Mexico, February 25-28, 2013."
320   $aIncludes bibliographical references (page 14).
606   $aAlkali metals$2nasat
606   $aCooling systems$2nasat
606   $aStirling cycle$2nasat
606   $aRadioisotope heat sources$2nasat
606   $aTime temperature parameter$2nasat
606   $aVenus atmosphere$2nasat
615  7$aAlkali metals.
615  7$aCooling systems.
615  7$aStirling cycle.
615  7$aRadioisotope heat sources.
615  7$aTime temperature parameter.
615  7$aVenus atmosphere.
700   $aSchwendeman$b Carl$01405441
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702782803321
996   $aAlkali metal backup cooling for Stirling systems, experimental results$93481942
997   $aUNINA

LEADER 02516oam  2200661I  450 
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101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue debonding characterization in composite skin/stringer configurations /$fMichael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center ;$aAlexandria, Virginia :$cU.S. Army Materiel Command,$dApril 1997.
215   $a1 online resource (33 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110331
225 1 $aU. S. Army Research Laboratory technical report ;$vARL-TR-1342
300   $a"April 1997."
300   $aTechnical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa.
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (page 12).
606   $aFatigue tests$2nasat
606   $aDebonding (materials)$2nasat
606   $aComposite structures$2nasat
606   $aFlanges$2nasat
606   $aSkin (structural member)$2nasat
606   $aBonded joints$2nasat
606   $aCrack initiation$2nasat
606   $aDelaminating$2nasat
606   $aGraphite-epoxy composites$2nasat
606   $aResin matrix composites$2nasat
615  7$aFatigue tests.
615  7$aDebonding (materials)
615  7$aComposite structures.
615  7$aFlanges.
615  7$aSkin (structural member)
615  7$aBonded joints.
615  7$aCrack initiation.
615  7$aDelaminating.
615  7$aGraphite-epoxy composites.
615  7$aResin matrix composites.
700   $aCvitkovich$b Michael$01423002
702   $aO'Brien$b T. Kevin
702   $aMinguet$b Pierre Jacques
712 02$aUnited States.$bArmy Materiel Command.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910708661003321
996   $aFatigue debonding characterization in composite skin$93549062
997   $aUNINA