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101 0 $aita$agrc
102   $aIT
105   $ay|||z|||001yy
200 1 $aJohannis Canani De Constantinopolis obsidione$fintroduzione, testo critico, traduzione e note a cura di Emilio Pinto
210   $aNapoli$cLibreria scientifica$d1968
215   $aXXVII, 46 p.$d26 cm
225 2 $aCollana di studi greci$v47
410  0$12001$aCollana di studi greci$v47
454  0$12001$aDiegesis peri tou en Kovstantinoupolei gegonotos polemou$918391
517 1 $aDe Constantinopolis obsidione
676   $a888.02
700  1$aCANANUS,$bIoannes$0616275
702  1$aPINTO,$bEmilio
801  0$aIT$bsalbc$gISBD
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951   $aXV.8. 936$b224426 L.M.$cXV.8.
959   $aBK
969   $aFSO
979   $aANNAMARIA$b90$c20130121$lUSA01$h0959
996   $aDiegesis peri tou en Kovstantinoupolei gegonotos polemou$918391
997   $aUNISA

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100   $a20130617d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOrion Pad Abort 1 Crew Module mass properties test approach and results /$fClaudia Herrera and Adam Harding
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d2012.
215   $a1 online resource (23 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-215995
300   $aTitle from title screen (viewed on June 17, 2013).
300   $a"March 2012."
320   $aIncludes bibliographical references (page 23).
606   $aCrew Exploration Vehicle$2nasat
606   $aLaunching pads$2nasat
606   $aAborted missions$2nasat
606   $aSpacecraft modules$2nasat
606   $aFlight tests$2nasat
606   $aMass distribution$2nasat
606   $aAerodynamic loads$2nasat
606   $aMoments of inertia$2nasat
606   $aDynamic structural analysis$2nasat
615  7$aCrew Exploration Vehicle.
615  7$aLaunching pads.
615  7$aAborted missions.
615  7$aSpacecraft modules.
615  7$aFlight tests.
615  7$aMass distribution.
615  7$aAerodynamic loads.
615  7$aMoments of inertia.
615  7$aDynamic structural analysis.
700   $aHerrera$b Claudia$01407951
702   $aHarding$b Adam
712 02$aHugh L. Dryden Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704472903321
996   $aOrion Pad Abort 1 Crew Module mass properties test approach and results$93490522
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