02338nam 2200613 450 991070462330332120130829094036.0(CKB)5470000002443485(OCoLC)857218783(EXLCZ)99547000000244348520130829d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierEntry, descent, and landing with propulsive deceleration supersonic retropropulsion wind tunnel testing /Bryan PalaszewskiCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (25 pages) illustrationsNASA/TM 2012-217746Title from title screen (viewed Aug. 29, 2013)."December 2012.""Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012..""AIAA-2012-401."Includes bibliographical references (pages 4-6).Entry, descent, and landing with propulsive deceleration Computational fluid dynamicsnasatPlanetary landingnasatAerodynamic brakesnasatLanding aidsnasatSoft landingnasatLanding sitesnasatRocket enginesnasatShock wave interactionnasatSupersonic flightnasatComputational fluid dynamics.Planetary landing.Aerodynamic brakes.Landing aids.Soft landing.Landing sites.Rocket engines.Shock wave interaction.Supersonic flight.Palaszewski Bryan Alan Richard1388221NASA Glenn Research Center,United States.National Aeronautics and Space Administration,AIAA Aerospace Sciences Meeting(50th :2012 :Nashville, Tenn.)GPOGPOBOOK9910704623303321Entry, descent, and landing with propulsive deceleration3529390UNINA