02515nam 2200673 a 450 991070075570332120120516092149.0(CKB)5470000002411450(OCoLC)793720770(EXLCZ)99547000000241145020120516d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierSpace Shuttle Program (SSP) orbiter main propulsion system (MPS) gaseous hydrogen (GH₂) flow control valve (FCV) poppet eddy current (EC) inspection probability of detection (POD) study[electronic resource] /Robert S. Piascik and Wiliam H. ProsserHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (2 volumes) illustrations (some color)NASA/TM ;2011-217072Title from title screen (viewed on May 16, 2012)."March 2011.""NESC-RP-09-00506."Includes bibliographical references.v. 1. [no distinct title] -- v. 2. Appendices.Space Shuttle Program Computational fluid dynamicsnasatNondestructive testsnasatControl valvesnasatSafetynasatSpace transportation systemnasatDynamic testsnasatHydrogennasatImpact testsnasatDetectionnasatEddy currentsnasatProbability theorynasatSpace Shuttle orbitersnasatComputational fluid dynamics.Nondestructive tests.Control valves.Safety.Space transportation system.Dynamic tests.Hydrogen.Impact tests.Detection.Eddy currents.Probability theory.Space Shuttle orbiters.Piascik Robert S1233573Prosser William H226019Langley Research Center.GPOGPOBOOK9910700755703321Space Shuttle Program (SSP) orbiter main propulsion system (MPS) gaseous hydrogen (GH₂) flow control valve (FCV) poppet eddy current (EC) inspection probability of detection (POD) study3534367UNINA