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    Titel :

    Parametric Study of an Ablative TPS and Hot Structure Heatshield for a Mars Entry Capsule Vehicle


    Beteiligte:

    Kongress:

    AIAA SPACE and Astronautics Forum and Exposition



    Erscheinungsdatum :

    2017-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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