01962nam 2200481 450 991070386030332120150715153515.0(CKB)5470000002435127(OCoLC)913834877(EXLCZ)99547000000243512720150715j198501 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierSpace shuttle orbiter trimmed center-of-gravity extension studyVolume ixEffects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 /W. Pelham Phillips and Roger H. FournierHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,January1985.1 online resource (97 pages) illustrationsNASA technical memorandum ;72661. vol. IXTitle from title screen (viewed July 15, 2015)."January1985."Includes bibliographical references (pages 10-11).Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5Aerodynamic characteristicsnasatCenter of gravitynasatSpace Shuttle orbitersnasatWind tunnel testsnasatCanard configurationsnasatAerodynamic characteristics.Center of gravity.Space Shuttle orbiters.Wind tunnel tests.Canard configurations.Phillips W. Pelham1416408Fournier Roger H.Langley Research Center,GPOGPOBOOK9910703860303321Space shuttle orbiter trimmed center-of-gravity extension study3521649UNINA