LEADER 02245nam  2200541 a 450 
001 9910700151003321
005 20110902163255.0
035   $a(CKB)5470000002407457
035   $a(OCoLC)748854918
035   $a(EXLCZ)995470000002407457
100   $a20110902d2010      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aHypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks$b[electronic resource] /$fHenry K. Nahra ... [and others] ; prepared for the 11th Hypervelocity Impact Symposium 2010 sponsored by the Hypervelocity Impact Society, Freiburg, Germany, April 11-15, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2010-216804
300   $aTitle from title screen (viewed on Sept. 2, 2011).
300   $a"October 2010."
320   $aIncludes bibliographical references (page 13).
606   $aHypervelocity impact$2nasat
606   $aMicromechanics$2nasat
606   $aResidual stress$2nasat
606   $aCrew Exploration Vehicle$2nasat
606   $aPropellant tanks$2nasat
606   $aService modules$2nasat
606   $aFabrication$2nasat
606   $aSpacecraft configurations$2nasat
615  7$aHypervelocity impact.
615  7$aMicromechanics.
615  7$aResidual stress.
615  7$aCrew Exploration Vehicle.
615  7$aPropellant tanks.
615  7$aService modules.
615  7$aFabrication.
615  7$aSpacecraft configurations.
701   $aNahra$b Henry K$01400461
712 02$aNASA Glenn Research Center.
712 12$aHypervelocity Impact Symposium$d(11th :$f2010 :$eFreiburg, Germany)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700151003321
996   $aHypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks$93515923
997   $aUNINA