02289nam 2200481 450 991070657950332120171204112855.0(CKB)5470000002456650(OCoLC)1012113929(EXLCZ)99547000000245665020171117j200101 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierStructural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit /Joseph M. Roche and Daniel N. KosareoCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,January 2001.1 online resource (10 pages) illustrationsNASA/TM ;2001-210667"January 2001.""Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.Includes bibliographical references (page 10).Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbitStructural sizing of a twenty-five thousand pound payload, air-breathing launch vehicle for single-state-to-orbitAir breathing boostersnasatReusable launch vehiclesnasatPropulsion system configurationsnasatSpace transportationnasatAir breathing boosters.Reusable launch vehicles.Propulsion system configurations.Space transportation.Roche Joseph M.1391265Kosareo Daniel NicholasNASA Glenn Research Center,GPOGPOBOOK9910706579503321Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit3464268UNINA