LEADER 01615nam  2200469I  450 
001 9910705706203321
005 20170711084054.0
035   $a(CKB)5470000002453350
035   $a(OCoLC)993259402
035   $a(EXLCZ)995470000002453350
100   $a20170710j201702    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aParametric structural model for a Mars entry concept /$fBrittney M. Lane and Samee W. Ahmed
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2017.
215   $a1 online resource (63 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219375
300   $a"February 2017."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 63).
606   $aAeroshells$2nasat
606   $aAtmospheric entry$2nasat
606   $aFinite element method$2nasat
606   $aMars environment$2nasat
606   $aSpacecraft launching$2nasat
615  7$aAeroshells.
615  7$aAtmospheric entry.
615  7$aFinite element method.
615  7$aMars environment.
615  7$aSpacecraft launching.
700   $aLane$b Brittney M.$01415248
702   $aAhmed$b Samee W.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705706203321
996   $aParametric structural model for a Mars entry concept$93516677
997   $aUNINA