LEADER 01690nam  2200493I  450 
001 9910705705803321
005 20170711083957.0
035   $a(CKB)5470000002453354
035   $a(OCoLC)993430824
035   $a(EXLCZ)995470000002453354
100   $a20170711j201706    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFinite element modeling and analysis of Mars entry aeroshell concept /$fSamee W. Ahmed, Brittney M. Lane
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 2017.
215   $a1 online resource (75 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2017-219374
300   $a"June 2017."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 53).
606   $aAerodynamics$2nasat
606   $aAeroshells$2nasat
606   $aAtmospheric entry$2nasat
606   $aFinite element method$2nasat
606   $aLift drag ratio$2nasat
606   $aMars atmosphere$2nasat
615  7$aAerodynamics.
615  7$aAeroshells.
615  7$aAtmospheric entry.
615  7$aFinite element method.
615  7$aLift drag ratio.
615  7$aMars atmosphere.
700   $aAhmed$b Samee W.$01409093
702   $aLane$b Brittney M.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705705803321
996   $aFinite element modeling and analysis of Mars entry aeroshell concept$93494647
997   $aUNINA