Overview of Low Density Supersonic Decelerator (LDSD) SFDT-2 ( Supersonic Flight Dynamics Test-2) flight profile; Description of Monte Carlo flight dynamics simulations performed; Modeling and uncertainties; Results with statistical prediction of test vehicle splashdown location; Use of Monte Carlo results for range safety and recovery planning.


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    Title :

    Construction of Supersonic Flight Dynamics Test (SFDT-2) Vehicle Monte Carlo Splashdown Footprints for Use in Range Safety and Recovery Planning


    Contributors:

    Conference:

    AAS/AIAA Space Flight Mechanics Meeting ; 2016 ; Napa, CA, United States


    Publication date :

    2016-02-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English







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