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:
    T. Polsgrove (author) / H. D. Thomas (author) / A. Dwyer Cianciolo (author) / T. Collins (author) / J. Samareh (author)

    Publication date :

    2017


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Mission and design sensitivities for human Mars landers using Hypersonic Inflatable Aerodynamic Decelerators

    Polsgrove, Tara P. / Thomas, Herbert D. / Cianciolo, Alicia Dwyer et al. | IEEE | 2017


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

    Polsgrove, Tara P. / Thomas, Herbert D. / Collins, Tim et al. | NTRS | 2017


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

    Polsgrove, Tara / Thomas, Herbert D. / Dwyer Cianciolo, Alicia et al. | NTRS | 2017



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

    Polsgrove, Tara P. / Thomas, Herbert D. / Dwyer Ciancio, Alicia et al. | NTRS | 2017