Develop two evolutionary rigid vehicle concepts to deliver human-scale payloads (20 metric tons) to the surface of Mars: Capsule; Lifting body, mid-range lift-to-drag ratio (Mid L/D). Determine vehicle configurations for various mission flight phases. Determine vehicle performance: Integrated system mass; Ability to meet landing constraints; Payload packaging and surface access. Provide technology investment recommendations to NASA’s Space Technology Mission Directorate.


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    Titel :

    Human Mars Entry, Descent and Landing Architecture Study (EDLAS): Rigid Decelerators


    Beteiligte:
    Polsgrove, Tara (Autor:in) / Percy, Thomas (Autor:in) / Garcia, Jay (Autor:in) / Dwyer Cianciolo, Alicia (Autor:in) / Samareh, Jamshid (Autor:in) / Lugo, Rafael (Autor:in) / Robertson, Ed (Autor:in) / Cerimele, Chris (Autor:in) / Sostaric, Ron (Autor:in)

    Kongress:

    Space and Astronautics Forum (AIAA SPACE Forum 2018) ; 2018 ; Orlando, FL, United States


    Erscheinungsdatum :

    17.09.2018


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Human Mars Entry, Descent, and Landing Architecture Study: Rigid Decelerators

    Polsgrove, Tara / Dwyer-Cianciolo, Alicia M. / Robertson, Edward A. et al. | AIAA | 2018


    Human Mars Entry, Descent and Landing Architecture Study: Rigid Decelerators

    Polsgrove, Tara P. / Percy, Thomas K. / Garcia, Jay C. et al. | NTRS | 2018


    HUMAN MARS ENTRY, DESCENT, AND LANDING ARCHITECTURE STUDY: RIGID DECELERATORS (AIAA 2018-5192)

    Polsgrove, Tara / Dwyer-Cianciolo, Alicia M. / Robertson, Edward A. et al. | British Library Conference Proceedings | 2018


    Human Mars Entry, Descent and Landing Architecture Study: Deployable Decelerators

    Dwyer Cianciolo, Alicia / Dillman, Robert / Brune, Andrew et al. | NTRS | 2019


    Human Mars Entry, Descent, and Landing Architecture Study: Deployable Decelerators

    Polsgrove, Tara / Percy, Thomas K. / Sutherlin, Steven et al. | AIAA | 2018