01956nam 2200541Ia 450 991069965360332120230902161817.0(CKB)5470000002404400(OCoLC)706732471(EXLCZ)99547000000240440020110310d2010 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSimplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware[electronic resource] /A.T. Nettles, A.J. Hodge, and J.R. Jackson[Huntsville], Ala. :National Aeronautics and Space Administration, Marshall Space Flight Center,[2010]1 online resource (27 pages) illustrationsNASA/TP ;2010-216434Title from title screen (viewed on March 10, 2011)."June 2010."Includes bibliographical references (pages 24-27).NASA technical paper ;216434.Composite materialsnasatCompression loadsnasatDegradationnasatDamagenasatFatigue (materials)nasatTolerances (mechanics)nasatFailurenasatComposite materials.Compression loads.Degradation.Damage.Fatigue (materials)Tolerances (mechanics)Failure.Nettles A. T(Alan T.)1389578Hodge A. J1403595Jackson J. R1403596George C. Marshall Space Flight Center.GPOGPOBOOK9910699653603321Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware3476580UNINA