01586nam 2200457 a 450 991070038230332120110825124449.0(CKB)5470000002409161(OCoLC)747836133(EXLCZ)99547000000240916120110825d2009 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierHot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications[electronic resource] /A.T. Nettles[Huntsville], Ala. :National Aeronautics and Space Administration, Marshall Space Flight Center,[2009]1 online resource (vii, 23 pages) illustrations (some color)NASA/TM ;2009-215900Title from title screen (viewed on Aug. 25, 2011)."June 2009."Includes bibliographical references (page 23).Epoxy matrix compositesnasatTemperature effectsnasatCompressive strengthnasatLaunch vehiclesnasatSafety factorsnasatEpoxy matrix composites.Temperature effects.Compressive strength.Launch vehicles.Safety factors.Nettles A. T(Alan T.)1389578George C. Marshall Space Flight Center.GPOGPOBOOK9910700382303321Hot3490401UNINA