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100   $a20110107d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEstimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods$b[electronic resource] /$fGary E. Erickson
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (v, 36 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216196
300   $aTitle from title screen (viewed on Jan. 7, 2011).
300   $a"February 2010."
320   $aIncludes bibliographical references (pages 23-24).
410  0$aNASA technical memorandum ;$v216196.
606   $aAerodynamic characteristics$2nasat
606   $aControl surfaces$2nasat
606   $aLaunch vehicles$2nasat
606   $aShock wave interaction$2nasat
606   $aSupersonic speed$2nasat
615  7$aAerodynamic characteristics.
615  7$aControl surfaces.
615  7$aLaunch vehicles.
615  7$aShock wave interaction.
615  7$aSupersonic speed.
700   $aErickson$b Gary E$01403144
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697041703321
996   $aEstimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods$93519399
997   $aUNINA