LEADER 02056nam  2200601   450 
001 9910704472803321
005 20130606165108.0
035   $a(CKB)5470000002440965
035   $a(OCoLC)846945158
035   $a(EXLCZ)995470000002440965
100   $a20130606d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aModeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas /$fParviz A. Bahrami
210  1$aMoffett Field, California :$cNational Aeronautics and Space Administration, Ames Research Center,$d2012.
215   $a1 online resource (iv, 13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-216006
300   $aTitle from title screen (viewed on June 6, 2013).
300   $a"March 2012."
320   $aIncludes bibliographical references (page 10).
606   $aAerobraking$2nasat
606   $aAerocapture$2nasat
606   $aAerodynamic heat transfer$2nasat
606   $aBallutes$2nasat
606   $aDrag devices$2nasat
606   $aSpacecraft reentry$2nasat
606   $aAerothermodynamics$2nasat
606   $aAtmospheric entry$2nasat
606   $aDescent trajectories$2nasat
606   $aMathematical models$2nasat
606   $aTrajectories$2nasat
615  7$aAerobraking.
615  7$aAerocapture.
615  7$aAerodynamic heat transfer.
615  7$aBallutes.
615  7$aDrag devices.
615  7$aSpacecraft reentry.
615  7$aAerothermodynamics.
615  7$aAtmospheric entry.
615  7$aDescent trajectories.
615  7$aMathematical models.
615  7$aTrajectories.
700   $aBahrami$b Parviz A$g(Parviz Ahmadi),$01411582
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704472803321
996   $aModeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas$93503216
997   $aUNINA