01749nam 2200457 450 991070796800332120170126153553.0(CKB)5470000002468887(OCoLC)970348771(EXLCZ)99547000000246888720170126j201607 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierDevelopment of constraint force equation methodology for application to multi-body dynamics including launch vehicle stage separation /Bandu N. Pamadi [and five others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,July 2016.1 online resource (xvi, 112 pages) illustrationsNASA/TP ;2016-219326"July 2016.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 111-112).Aerodynamic forcesnasatBooster rocket enginesnasatLaunch vehiclesnasatOrbit insertionnasatStage separationnasatAerodynamic forces.Booster rocket engines.Launch vehicles.Orbit insertion.Stage separation.Pamadi Bandu N.1945-727368Langley Research Center,GPOGPOBOOK9910707968003321Development of constraint force equation methodology for application to multi-body dynamics including launch vehicle stage separation3520261UNINA