[Note: this is the presentation for a companion paper with the following abstract] The National Aeronautics and Space Administration’s (NASA) Mars Architecture Team (MAT) was challenged to develop a mission architecture capable of transporting humans to the surface of Mars and back as fast—and as soon—as practical. This challenge represented a significant departure from previous approaches that minimized Earth-launched mass and maximized in-space transportation efficiency, often resulting in roundtrip missions of three years or more in duration. In the interest of crew health, MAT’s cross-Agency team of subject matter experts was challenged to develop an architecture capable of shortening crew time away from Earth to about two years. MAT was given specific mission constraints, such as number of crew, as well as mandates to minimize surface infrastructure as much as possible and to incorporate nuclear transportation options. The resulting MAT-developed concept, referred to here as the Strategic Analysis Cycle 2021 (SAC21) architecture, leverages Artemis elements and emerging commercial capabilities for cargo and logistics launches, and features a hybrid Nuclear Electric Propulsion (NEP)/Chemical transportation system able to complete the 1.8 billion kilometer round-trip journey to Mars and back in 760 to 850 days transit time for the 2039 Earth departure opportunity. Three Mars Descent Systems (MDS), each capable of landing about 25 metric tons of useful cargo on the surface of Mars, would be pre-deployed in advance of crew departure from Earth; two of these MDS’s would deliver a partially fueled Mars Ascent Vehicle (MAV), a fission power system, surface mobility, and additional MAV propellant. To minimize surface infrastructure, only two of the four Mars crew would descend and live in an MDS-landed pressurized rover, exploring the martian surface for 30 martian days, or sols, before returning to Mars orbit aboard their MAV and rejoining the other two crew on the Deep Space Transport for the Earth return voyage. Specifics of many of these architecture elements are detailed in separate technical publications; this paper outlines the end-to-end integrated architecture performance and concept of operations, including synergies with Artemis lunar architecture elements. It is important to note that NASA does not have a formal human Mars program and no decisions have been made; the architecture described here is intended to fill in an often-overlooked corner of the trade space, helping to complete the menu of options available to decision-makers as they chart the course for humans to Mars. Note: Slide 9 contains a ~2 min video, best viewed when downloaded. Once downloaded to begin video you may be requested to hit options and Trust this document.


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    Titel :

    NASA’s Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture


    Beteiligte:
    Michelle Rucker (Autor:in) / Douglas A Craig (Autor:in) / Laura M Burke (Autor:in) / Patrick R Chai (Autor:in) / Michael B Chappell (Autor:in) / Bret G Drake (Autor:in) / Stephen J Edwards (Autor:in) / Stephen Hoffman (Autor:in) / Andrew C McCrea (Autor:in) / Douglas J Trent (Autor:in)

    Kongress:

    IEEE Aerospace Conference ; 2022 ; Big Sky, MT, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    NASA's Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture

    Rucker, Michelle A. / Craig, Douglas A. / Burke, Laura M. et al. | IEEE | 2022


    NASA’s Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture

    M. Rucker / D. A. Craig / L. M. Burke et al. | NTIS | 2022


    NASA’s Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture

    Michelle A Rucker / Douglas A Craig / Laura M Burke et al. | NTRS | 2022


    Updated Human Mars Ascent Vehicle Concept in Support of NASA's Strategic Analysis Cycle 2021

    Trent, Douglas J. / Thomas, Herbert D. / Rucker, Michelle A. | IEEE | 2022