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  • MISSION ARCHITECTURE AND TECHNOLOGY OPTIONS FOR A FLAGSHIP CLASS VENUS IN SITU MISSION

    Paper number

    IAC-08.A3.6.9

    Author

    Dr. Tibor S. Balint, Jet Propulsion Laboratory, United States

    Coauthor

    Dr. Elizabeth A. Kolawa, Jet Propulsion Laboratory, United States

    Coauthor

    Dr. James A. Cutts, Jet Propulsion Laboratory, United States

    Coauthor

    Dr. David Senske, Jet Propulsion Laboratory, United States

    Coauthor

    Dr. Johnny Kwok, Jet Propulsion Laboratory, United States

    Year

    2008

    Abstract
    Venus, as part of the inner triad with Earth and Mars, represents an important exploration target if we want to learn more about solar system formation and evolution. Comperative planetology could also elucidate the differences between the past, present, and future of these three planets, and can help with the characterization of potential habitable zones in our solar system and, by extension, extra-solar systems. A long-lived in situ Venus mission concept, called the Venus Mobile Explorer, was prominently featured in NASA’s 2006 SSE Roadmap and supported in the community White Paper by the Venus Exploration Analysis Group (VEXAG). Long-lived in situ missions are expected to belong to the largest (Flagship) mission class, which would require both enabling and enhancing technologies beside mission architecture options. Furthermore, extreme environment mitigation technologies for Venus are considered long lead development items and are expected to require technology development through a dedicated program. To better understand programmatic and technology needs and the motivating science behind them, in this fiscal year (FY08) NASA is funding a Venus Flaghip class mission study, based on key science and technology drivers identified by a NASA appointed Venus Science and Technology Definition Team (STDT). These mission drivers are then assembled around a suitable mission architecture to further refine technology and cost elements. In this paper we will discuss the connection between the final mission architecture and the connected technology drivers from this NASA funded study, which - if funded - could enable a future Flagship class Venus mission and potentially drive a proposed Venus technology development program.
    Abstract document

    IAC-08.A3.6.9.pdf

    Manuscript document

    IAC-08.A3.6.9.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.