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100   $a20170202j199302    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic Aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration /$fGeorge M. Ware and Charles H. Fox, Jr
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dFebruary 1993.
215   $a1 online resource (27 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4439
300   $a"February 1993" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 4-5).
606   $aAngle of attack$2nasat
606   $aDelta wings$2nasat
606   $aReusable launch vehicles$2nasat
606   $aRolling moments$2nasat
606   $aSpace transportation system$2nasat
606   $aYawing moments$2nasat
615  7$aAngle of attack.
615  7$aDelta wings.
615  7$aReusable launch vehicles.
615  7$aRolling moments.
615  7$aSpace transportation system.
615  7$aYawing moments.
700   $aWare$b George M.$01410132
702   $aFox$b Charles H.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707952903321
996   $aSubsonic Aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration$93514251
997   $aUNINA