01615nam 2200469I 450 991070570620332120170711084054.0(CKB)5470000002453350(OCoLC)993259402(EXLCZ)99547000000245335020170710j201702 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierParametric structural model for a Mars entry concept /Brittney M. Lane and Samee W. AhmedHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,February 2017.1 online resource (63 pages) color illustrationsNASA/TM ;2017-219375"February 2017.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 63).AeroshellsnasatAtmospheric entrynasatFinite element methodnasatMars environmentnasatSpacecraft launchingnasatAeroshells.Atmospheric entry.Finite element method.Mars environment.Spacecraft launching.Lane Brittney M.1415248Ahmed Samee W.Langley Research Center,GPOGPOBOOK9910705706203321Parametric structural model for a Mars entry concept3516677UNINA