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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    Title :

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


    Contributors:

    Conference:

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


    Publication date :

    2017-03-07


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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