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  • Some necessary technologies for in-situ astrobiology on Enceladus

    Paper number

    IAC-15,A3,IP,8,x29537

    Author

    Mr. Konstantinos Konstantinidis, Universität der Bundeswehr München, Germany

    Coauthor

    Dr. Julia Kowalski, FH Aachen University of Applied Sciences, Germany

    Coauthor

    Mr. Claudio Flores Martinez, University of Heidelberg, Germany

    Coauthor

    Prof. Bernd Dachwald, FH Aachen University of Applied Sciences, Germany

    Coauthor

    Prof.Dr. Roger Förstner, Universität der Bundeswehr München, Germany

    Coauthor

    Mr. Dirk Ewerhart, Germany

    Year

    2015

    Abstract
    The plumes discovered by the Cassini mission emanating from the south pole of Saturn's moon Enceladus and the unique chemistry found in them have fueled speculations that Enceladus may harbor life. The presumed water-filled cracks from which the plumes emanate would make a prime target in the search for extraterrestrial life and would be more easily accessible than the moon's subglacial ocean. A lander mission that is equipped with a subsurface maneuverable ice melting probe will be most suitable to assess the existence of life on Enceladus. A lander would have to land at a safe distance away from a plume source and use a melting probe to melt to the inner wall of the crack to analyze the plume subsurface liquids before potential biosignatures are degraded or destroyed by exposure to the vacuum of space.
    
    A concept study for such a lander mission was performed as part of the “Enceladus Explorer” (EnEx) project funded by the German Space Administration (DLR). During this study some key technologies for such a mission were identified, and will be discussed in this paper:
    
    1. The mission includes two critical operational phases: a descent and landing phase with pinpoint accuracy, and a subglacial melting phase where the melting probe must navigate and maneuver to the side of the target water filled crack at a certain depth to sample the water there. Guidance, Navigation and Control systems are presented for both the lander and the melting probe, as well as autonomy concepts for their operation.
    
    2. Due to the high power demand for melting the cold ice on an icy moon, high density power sources are necessary. At the same time, future planetary protection regulations will likely restrict or prohibit landing nuclear power sources near astrobiologically interesting areas for fear of contamination. Here, both small nuclear reactors and high density hydrogen fuels cells are discussed as candidate power sources, their technological maturity is assessed and future development steps are proposed.
    
    3. Several instruments can be conceivably used to detect biosignatures in-situ: antibody microarrays, nanopore-based devices, microscopes, flow cytometers, fatty acid markers, and mass spectrometers. However technological maturity and capability for miniaturization vary between each instrument type. Here we propose a way forward for the development of such suitable miniaturized instruments for in-situ icy moon astrobiology.
    Abstract document

    IAC-15,A3,IP,8,x29537.brief.pdf

    Manuscript document

    IAC-15,A3,IP,8,x29537.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.