01790nam 2200481 a 450 991070115660332120111128133927.0(CKB)5470000002415481(OCoLC)763304966(EXLCZ)99547000000241548120111128d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierEvaluation of aluminum alloy 2050-T84 microstructure and mechanical properties at ambient and cryogenic temperatures[electronic resource] /Robert A. Hafley ... [and others]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (viii, 70 pages) illustrations (chiefly color)NASA/TM ;2011-217163Title from title screen (viewed on Nov. 28, 2011)."July 2011."Includes bibliographical references (pages 16-17).Aluminum alloysnasatCompression testsnasatCryogenic temperaturenasatHeavy lift launch vehiclesnasatTensile testsnasatPropellant tanksnasatAluminum alloys.Compression tests.Cryogenic temperature.Heavy lift launch vehicles.Tensile tests.Propellant tanks.Hafley Robert A1396787Langley Research Center.GPOGPOBOOK9910701156603321Evaluation of aluminum alloy 2050-T84 microstructure and mechanical properties at ambient and cryogenic temperatures3510435UNINA