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100   $a20160223j199607    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle /$fRoger A. Lepsch, Jr. and George M. Ware, Ian 0. MacConochie
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 1996.
215   $a1 online resource (29 pages.) $cillustrations
225 1 $aNASA technical memorandum ;$v4726
300   $aTitle from title screen (viewed on Feb. 23, 2016).
300   $a"July 1996."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aWind tunnel tests$2nasat
606   $aSpace transportation system$2nasat
606   $aSingle stage to orbit vehicles$2nasat
606   $aReusable spacecraft$2nasat
606   $aLift drag ratio$2nasat
615  7$aWind tunnel tests.
615  7$aSpace transportation system.
615  7$aSingle stage to orbit vehicles.
615  7$aReusable spacecraft.
615  7$aLift drag ratio.
700   $aLepsch$b Roger A.$01402583
702   $aWare$b George M.
702   $aMacConochie$b Ian O.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704399003321
996   $aSubsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle$93473432
997   $aUNINA