01884nam 2200505 a 450 991070185330332120120622101917.0(CKB)5470000002421575(OCoLC)796083014(EXLCZ)99547000000242157520120622d2011 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierA damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications[electronic resource] /A.T. NettlesHuntsville, Ala. :National Aeronautics and Space Administration, Marshall Space Flight Center,[2011]1 online resource (vii, 39 pages) illustrations (some color)NASA/TM ;2011-216477Title from title screen (viewed on June 22, 2012)."December 2011."Includes bibliographical references (page 39).Compressive strengthnasatImpact strengthnasatHoneycomb structuresnasatLaunch vehiclesnasatDamagenasatTolerances (mechanics)nasatResidual strengthnasatCompressive strength.Impact strength.Honeycomb structures.Launch vehicles.Damage.Tolerances (mechanics)Residual strength.Nettles A. T(Alan T.)1389578George C. Marshall Space Flight Center.GPOGPOBOOK9910701853303321A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications3492436UNINA