02056nam 2200601 450 991070447280332120130606165108.0(CKB)5470000002440965(OCoLC)846945158(EXLCZ)99547000000244096520130606d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierModeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas /Parviz A. BahramiMoffett Field, California :National Aeronautics and Space Administration, Ames Research Center,2012.1 online resource (iv, 13 pages) color illustrationsNASA/TM ;2012-216006Title from title screen (viewed on June 6, 2013)."March 2012."Includes bibliographical references (page 10).AerobrakingnasatAerocapturenasatAerodynamic heat transfernasatBallutesnasatDrag devicesnasatSpacecraft reentrynasatAerothermodynamicsnasatAtmospheric entrynasatDescent trajectoriesnasatMathematical modelsnasatTrajectoriesnasatAerobraking.Aerocapture.Aerodynamic heat transfer.Ballutes.Drag devices.Spacecraft reentry.Aerothermodynamics.Atmospheric entry.Descent trajectories.Mathematical models.Trajectories.Bahrami Parviz A(Parviz Ahmadi),1411582NASA Glenn Research Center,GPOGPOBOOK9910704472803321Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas3503216UNINA