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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    Strauss, Bill (Autor:in) / Ivanov, Mark (Autor:in)

    Kongress:

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


    Erscheinungsdatum :

    2016-02-15


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch







    SEPARATION DEVICE FOR MARINE RECOVERY AND SPLASHDOWN

    Europäisches Patentamt | 2020

    Freier Zugriff

    SEPARATION DEVICE FOR MARINE RECOVERY AND SPLASHDOWN

    KWANJUNG YEE / GYUJIN SHIM / JUNGPYO KANG et al. | Europäisches Patentamt | 2020

    Freier Zugriff