The simulation tools and processes used to generate aerothermodynamic environment definitions for the Mars 2020 entry capsule are presented. The Mars 2020 capsule leverages the heritage Mars Science Laboratory design, but the entry will follow a different trajectory, landing at a different location and altitude on Mars. The general strategy for creating the Mars 2020 mission-specific environments follows from the Mars Science Laboratory experience. The primary difference is that now the effects of shock-layer radiation are modeled, with particular concern for the backshell.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule


    Beteiligte:

    Kongress:

    2018 AIAA Aviation Forum ; 2018 ; Atlanta, GA, United States


    Erscheinungsdatum :

    25.06.2018


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule

    Wise, Adam / Prabhu, Dinesh K. / Johnston, Christopher O. et al. | AIAA | 2018


    Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule (AIAA 2018-3116)

    Wise, Adam / Prabhu, Dinesh K. / Johnston, Christopher O. et al. | British Library Conference Proceedings | 2018


    Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule

    Edquist, Karl T. / Dyakonov, Artem A. / Wright, Michael J. et al. | NTRS | 2007


    Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule

    Edquist, Karl / Dyakonov, Artem / Wright, Michael et al. | AIAA | 2007


    Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule AIAA Paper

    Edquist, K. / Dyakonov, A. / Wright, M. et al. | British Library Conference Proceedings | 2007