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  • Lunar Excavator: Regolith Mining Operations Testing

    Paper number

    IAC-19,A3,IP,11,x54554

    Author

    Mr. Jason Schuler, United States, National Aeronautics and Space Administration (NASA)

    Coauthor

    Mr. Jonathan Smith, United States, National Aeronautics and Space Administration (NASA)

    Coauthor

    Mr. Kurt Leucht, United States, National Aeronautics and Space Administration (NASA)

    Coauthor

    Mr. Andrew Nick, United States

    Coauthor

    Mr. Buckles Bradley, United States

    Year

    2019

    Abstract
    Regolith is the primary resource available to enable a sustained presence on the lunar surface. We will need to mine thousands of metric tons of regolith for propellant production, water, construction material, and more. However, to date robotic vehicles have only collected small samples. To overcome this we will need to develop and test a new class of space robot that must perform a series of operations never attempted on another planetary body before.
    
    The purpose of this paper is to discuss the validation testing of a prototype robotic lunar excavator. The Regolith Advanced Surface Systems Operations Robot (RASSOR) is a 67kg robot that is designed to mine regolith in reduced gravity. A notional in-situ resource utilization (ISRU) technology demonstration with a goal of producing 10mT of oxygen in 1 year was selected as the design reference mission (DRM).
    
    The DRM was used to develop a concept of operations for RASSOR. Each operation was performed at the Kennedy Space Center in a lunar regolith testbed filled with 120mT of simulant. Time, energy, and visual data were recorded for each operation. Some of the tested operations included: driving 100m with and without a regolith payload, excavating, delivering regolith into a hopper, building a ramp, building a berm, and contingency operations. 
    
    The testing demonstrated that RASSOR is capable the completing necessary operations for the DRM. This paper will discuss the time and energy usage for the various operations and compare the results to model based predictions. Photographs of the operations and lessons learned will be presented. These results will be used to inform future mission planning and, if selected, a protoflight version of RASSOR will be developed and appropriate lifetime and flight qualification testing will be completed.
    Abstract document

    IAC-19,A3,IP,11,x54554.brief.pdf

    Manuscript document

    (absent)