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  • Mars Prospector: Leading the way to in-situ resource utilization on the Red Planet

    Paper number

    IAC-18,D3,3,1,x47522

    Author

    Mr. Fabrizio Bernardini, Italy, Planetary Science Institute

    Coauthor

    Mr. Wayne Sidney, United States, Laboratory for Atmospheric and Space Physics (LASP) at University of Colorado

    Coauthor

    Dr. Angel Abbud-Madrid, United States, Colorado School of Mines

    Coauthor

    Dr. Nathaniel Putzig, United States, Planetary Science Institute

    Coauthor

    Dr. Roger Clark, United States, Planetary Science Institute

    Coauthor

    Mr. Matthew Perry, United States, Planetary Science Institute

    Coauthor

    Prof. Isaac Smith, United States, Planetary Science Institute

    Year

    2018

    Abstract
    With the growing prospect of humans once again venturing beyond Earth orbit to establish planetary outposts, the identification and assessment of in-situ resources at planned destinations is paramount. Currently, opportunities for assessing such resources depend on space-agency planning and mission cycles that generally focus on science return rather than addressing a specific need. We present a novel concept for rapidly implementing a resource-prospecting orbiter using a spacecraft bus and instruments already at high technology readiness levels (TRL). 
    
    The Mars Prospector mission concept is focused on assessing known but not adequately characterized resources for utilization at future human landing sites on the Red Planet. The mission is designed around the spacecraft bus being built by the University of Colorado’s Laboratory for Atmospheric and Space Physics (LASP) for the Emirates Mars Mission (EMM). Two primary instruments are a multi-band radar sounder that will assess the presence, depth, and concentration of buried water ice and an imaging spectrometer that will identify and map hydrated minerals amenable to extraction of water. All components are to be derived from existing hardware, reducing the risks and long development times normally associated with science-focused missions. In addition, by concentrating the mission goals on prospecting in well-defined areas, we will reduce the typical far-reaching requirements for planetary orbiters, thereby simplifying engineering, integration, and operations. 
    
    The multi-band radar is derived from current Mars sounders, modified to provide resolutions that are sub-meter vertically and sub-kilometer horizontally. These updates are intended to establish the lateral extent and resolve the top and bottom of buried ground ices thought to exist in large regions of Mars’ northern plains. They also enable characterization of the debris and its thickness covering glaciers in the mid-latitudes of both hemispheres in locations accessible from future human landing sites.
     
    The imaging spectrometer design will be focused primarily on identifying and mapping hydrated minerals, but it will also allow thermal measurements for assessing physical properties of surface materials. By narrowly constraining the instrument goals in this fashion, a number of current, relatively low-cost spectrometers could be adapted to provide the bandwidth, spectral and spatial resolutions, and accuracy needed for these purposes.
    
    The Mars Prospector mission concept is modular, allowing different instruments to be affixed to the LASP/EMM bus. This feature opens the door for potential follow-on missions to the Moon, back to Mars, or to small bodies of interest for resource assessment and prospecting.
    Abstract document

    IAC-18,D3,3,1,x47522.brief.pdf

    Manuscript document

    IAC-18,D3,3,1,x47522.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.