01890nam 2200505 450 991070273380332120150203124318.0(CKB)5470000002430863(OCoLC)902679849(EXLCZ)99547000000243086320150203j201409 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites a protocol for producing void-free quality laminates /Tan-Hung HouHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 2014.1 online resource (16 pages) illustrationsNASA/TM ;2014-218524Title from title screen (viewed Feb. 3, 2015)."September 2014."Includes bibliographical references (pages 15-16).Cure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites Resin matrix compositesnasatLaminatesnasatPressure distributionnasatVoidsnasatMatrix materialsnasatPolyimidesnasatResin matrix composites.Laminates.Pressure distribution.Voids.Matrix materials.Polyimides.Hou T. H.1393498Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702733803321Cure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites3449691UNINA