LEADER 01949nam  2200565I  450 
001 9910704472903321
005 20130617105843.0
035   $a(CKB)5470000002440964
035   $a(OCoLC)848834196
035   $a(EXLCZ)995470000002440964
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
997   $aUNINA