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100   $a20150715j198501    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSpace shuttle orbiter trimmed center-of-gravity extension study$hVolume ix$iEffects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 /$fW. Pelham Phillips and Roger H. Fournier
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary1985.
215   $a1 online resource (97 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v72661. vol. IX
300   $aTitle from title screen (viewed July 15, 2015).
300   $a"January1985."
320   $aIncludes bibliographical references (pages 10-11).
517 3 $aEffects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5
606   $aAerodynamic characteristics$2nasat
606   $aCenter of gravity$2nasat
606   $aSpace Shuttle orbiters$2nasat
606   $aWind tunnel tests$2nasat
606   $aCanard configurations$2nasat
615  7$aAerodynamic characteristics.
615  7$aCenter of gravity.
615  7$aSpace Shuttle orbiters.
615  7$aWind tunnel tests.
615  7$aCanard configurations.
700   $aPhillips$b W. Pelham$01416408
702   $aFournier$b Roger H.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703860303321
996   $aSpace shuttle orbiter trimmed center-of-gravity extension study$93521649
997   $aUNINA