Entry, Descent and Landing (EDL) Modeling and Simulation (MS) is an enabling capability for complex NASA entry missions such as MSL and Orion. MS is used in every mission phase to define mission concepts, select appropriate architectures, design EDL systems, quantify margin and risk, ensure correct system operation, and analyze data returned from the entry. In an environment where it is impossible to fully test EDL concepts on the ground prior to use, accurate MS capability is required to extrapolate ground test results to expected flight performance.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Predictive Modeling for NASA Entry, Descent and Landing Missions


    Contributors:

    Conference:

    The International Conference for High Performance Computing, Networking, Storage and Analysis (SC16) ; 2016 ; Salt Lake City, UT, United States


    Publication date :

    2016-11-13


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Aerothermal Modeling Challenges for Entry Descent and Landing Missions

    Wright, Michael J. / Hollis, Brian R. / Barnhardt, Michael D. et al. | NTRS | 2018


    Entry, Descent, and Landing for Human Mars Missions

    Munk, Michelle M. / DwyerCianciolo, Alicia M. | NTRS | 2012


    Entry descent and landing systems for future missions

    Anselmo, Luciano | Online Contents | 2010


    Entry, Descent, and Landing for Human Mars Missions

    M. M. Munk / A. M. DwyerCianciolo | NTIS | 2012


    Overview of the NASA Entry, Descent and Landing Systems Analysis Studies for Large Robotic-class Missions

    Zang, Thomas / Dwyer-Cianciolo, Alicia / Ivanov, Mark et al. | AIAA | 2011