02035nam 2200553Ia 450 991070076080332120110823113036.0(CKB)5470000002411398(OCoLC)747568690(EXLCZ)99547000000241139820110823d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage[electronic resource] /A.J. Hodge, A.T. Nettles, and J.R. Jackson[Huntsville], Ala. :National Aeronautics and Space Administration, Marshall Space Flight Center,[2011]1 online resource (viii, 23 pages) illustrations (some color)NASA/TP ;2011-216460Title from title screen (viewed on Aug. 22, 2011)."March 2011."Includes bibliographical references (pages 22-23).Compressive strengthnasatSandwich structuresnasatCarbon fibersnasatImpact strengthnasatDamagenasatEpoxy matrix compositesnasatLaminatesnasatFiber compositesnasatCompressive strength.Sandwich structures.Carbon fibers.Impact strength.Damage.Epoxy matrix composites.Laminates.Fiber composites.Hodge A. J1403595Nettles A. T(Alan T.)1389578Jackson J. R1403596George C. Marshall Space Flight Center.GPOGPOBOOK9910700760803321Comparison of open-hole compression strength and compression after impact strength on carbon fiber3498703UNINA