01577oam 2200433 450 991071716310332120220218085610.0(CKB)5470000002528584(OCoLC)1293754032(EXLCZ)99547000000252858420220126j202201 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierA quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure /A.T. Nettles, W.E. Guin, and C.C. WolfeHuntsville, Alabama :National Aeronautics and Space Administration, Marshall Space Flight Center,January 2022.1 online resource (approximately 30 pages) illustrations (some color)NASA/TM ;20210026811"January 2022."Includes bibliographical references (page 17).Composite materialsnasatSandwich structuresnasatCarbon fibersnasatComposite materials.Sandwich structures.Carbon fibers.Nettles A. T(Alan T.),1389578Guin W. E.Wolfe C. C.George C. Marshall Space Flight Center,GPOGPOGPOBOOK9910717163103321A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure3476814UNINA