02245nam 2200541 a 450 991070015100332120110902163255.0(CKB)5470000002407457(OCoLC)748854918(EXLCZ)99547000000240745720110902d2010 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierHypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks[electronic resource] /Henry K. Nahra ... [and others] ; prepared for the 11th Hypervelocity Impact Symposium 2010 sponsored by the Hypervelocity Impact Society, Freiburg, Germany, April 11-15, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (13 pages) color illustrationsNASA/TM ;2010-216804Title from title screen (viewed on Sept. 2, 2011)."October 2010."Includes bibliographical references (page 13).Hypervelocity impactnasatMicromechanicsnasatResidual stressnasatCrew Exploration VehiclenasatPropellant tanksnasatService modulesnasatFabricationnasatSpacecraft configurationsnasatHypervelocity impact.Micromechanics.Residual stress.Crew Exploration Vehicle.Propellant tanks.Service modules.Fabrication.Spacecraft configurations.Nahra Henry K1400461NASA Glenn Research Center.Hypervelocity Impact Symposium(11th :2010 :Freiburg, Germany)GPOGPOBOOK9910700151003321Hypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks3515923UNINA