01949nam 2200565I 450 991070447290332120130617105843.0(CKB)5470000002440964(OCoLC)848834196(EXLCZ)99547000000244096420130617d2012 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierOrion Pad Abort 1 Crew Module mass properties test approach and results /Claudia Herrera and Adam HardingEdwards, CA :National Aeronautics and Space Administration, Dryden Flight Research Center,2012.1 online resource (23 pages) illustrations (some color)NASA/TM ;2012-215995Title from title screen (viewed on June 17, 2013)."March 2012."Includes bibliographical references (page 23).Crew Exploration VehiclenasatLaunching padsnasatAborted missionsnasatSpacecraft modulesnasatFlight testsnasatMass distributionnasatAerodynamic loadsnasatMoments of inertianasatDynamic structural analysisnasatCrew Exploration Vehicle.Launching pads.Aborted missions.Spacecraft modules.Flight tests.Mass distribution.Aerodynamic loads.Moments of inertia.Dynamic structural analysis.Herrera Claudia1407951Harding AdamHugh L. Dryden Flight Research Center,GPOGPOBOOK9910704472903321Orion Pad Abort 1 Crew Module mass properties test approach and results3490522UNINA