This paper explores the impact of human Mars mission architecture decisions on the design and performance of a lander using the HIAD entry system: (a) Earth departure options, (b) Mars arrival options, (c) Entry Descent and Landing options.


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    Titel :

    Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators


    Beteiligte:

    Kongress:

    IEEE Aerospace Conference ; 2017 ; Big Sky, MT, United States


    Erscheinungsdatum :

    07.03.2017


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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