02169nam 2200577Ia 450 991070076110332120110802115112.0(CKB)5470000002411395(OCoLC)744420941(EXLCZ)99547000000241139520110802d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles[electronic resource] /A.T. Nettles, A.J. Hodge, and J.R. Jackson[Huntsville], Ala. :National Aeronautics and Space Administration, Marshall Space Flight Center,[2011]1 online resource (vii, 23 pages) illustrationsNASA/TP ;2011-216457Title from title screen (viewed on Aug. 2, 2011)."February 2011."Includes bibliographical references (pages 22-23).Damage assessmentnasatLaunch vehiclesnasatThermal protectionnasatSandwich structuresnasatResidual strengthnasatAres 1 launch vehiclenasatComposite structuresnasatComposite materialsnasatImpact damagenasatDamage assessment.Launch vehicles.Thermal protection.Sandwich structures.Residual strength.Ares 1 launch vehicle.Composite structures.Composite materials.Impact damage.Nettles A. T(Alan T.)1389578Hodge A. J1403595Jackson J. R1403596George C. Marshall Space Flight Center.GPOGPOBOOK9910700761103321The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles3551009UNINA