01840oam 2200529I 450 991070613350332120170911090326.0(CKB)5470000002455094(OCoLC)858242490(EXLCZ)99547000000245509420130912j199909 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierCyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept /H. Kevin RiversHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 1999.1 online resource (13 pages) illustrationsNASA/TM ;1999-209560"September 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 11).Cyclic cryogenic thermal-mechanical testing of an X-33 reusable launch vehicle liquid oxygen tank concept7Cyclic loadsnasatStorage tanksnasatPropellant tanksnasatLoad testsnasatLoad testing machinesnasatFlight simulationnasat7Cyclic loads.Storage tanks.Propellant tanks.Load tests.Load testing machines.Flight simulation.Rivers H. Kevin1419508Langley Research Center,OCLCEOCLCEOCLCOOCLCQGPOBOOK9910706133503321Cyclic cryogenic thermal-mechanical testing of an X-333534252UNINA