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  • LUVMI: an innovative payload for the sampling of volatiles at the Lunar poles

    Paper number

    IAC-17,A3,2B,10,x41392

    Author

    Mr. Diego A. Urbina, Space Applications Services N.V./S.A, Belgium

    Coauthor

    Dr. Jeremi Gancet, Space Applications Services N.V., Belgium

    Coauthor

    Mr. Karsten Kullack, Space Applications Services N.V./S.A, The Netherlands

    Coauthor

    Mr. Enrico Ceglia, Space Applications Services N.V./S.A, The Netherlands

    Coauthor

    Mr. Hemanth Kumar Madakashira, Space Applications Services N.V./S.A, Belgium

    Coauthor

    Mr. Joseph Salini, Space Applications Services N.V./S.A., Belgium

    Coauthor

    Mr. Shashank Govindaraj, Space Applications Services N.V./S.A, Belgium

    Coauthor

    Mr. Leonardo Surdo, Space Applications Services N.V./S.A, The Netherlands

    Coauthor

    Dr. Simeon Barber, Open University, United Kingdom

    Coauthor

    Dr. Simon Sheridan, Open University, United Kingdom

    Coauthor

    Ms. Janos Biswas, Technische Universität München, Germany

    Coauthor

    Mr. Philipp Reiss, Technische Universität München, Germany

    Coauthor

    Dr. Neil Murray, Dynamic Imaging Analytics, United Kingdom

    Coauthor

    Dr. Anthony Evangora, Dynamic Imaging Analytics, United Kingdom

    Coauthor

    Mr. Joseph Rushton, Dynamic Imaging Analytics, United Kingdom

    Coauthor

    Mr. Lutz Richter, OHB System AG, Germany

    Coauthor

    Ms. Diana Dobrea, OHB System AG - Munich, Germany

    Coauthor

    Mr. Mattia Reganaz, OHB System AG, Germany

    Coauthor

    Mr. Richard Aked, Space Applications Services N.V./S.A, Belgium

    Coauthor

    Mr. Craig Pitcher, United Kingdom

    Year

    2017

    Abstract
    The ISECG identifies one of the first exploration steps as in situ investigations of the moon or asteroids. Europe is developing payload concepts for drilling and sample analysis, a contribution to a 250kg rover as well as for sample return. To achieve these missions, ESA depends on international partnerships.
    
    Such missions will be seldom, expensive and the drill/sample site selected will be based on observations from orbit not calibrated with ground truth data.
    Many of the international science community’s objectives can be met at lower cost, or the chances of mission success improved and the quality of the science increased by making use of an innovative, low mass, mobile robotic payload following the LEAG recommendations.
    
    LUVMI provides a smart, low mass, innovative, modular mobile payload comprising surface and sub-surface sensing with an in-situ sampling technology capable of depth-resolved extraction of volatiles, combined with a volatile analyser (mass spectrometer) capable of identifying the chemical composition of the most important volatiles. This will allow LUVMI to: traverse the lunar surface prospecting for volatiles; sample subsurface up to a depth of 10 cm (with a goal of 20 cm); extract water and other loosely bound volatiles; identify the chemical species extracted; access and sample permanently shadowed regions (PSR).
    
    The main innovation of LUVMI is to develop an in situ sampling technology capable of depth-resolved extraction of volatiles, and then to package within this tool, the analyser itself, so as to maximise transfer efficiency and minimise sample handling and its attendant mass requirements and risk of sample alteration. By building on national, EC and ESA funded research and developments, this project will develop to TRL6 instruments that together form a smart modular mobile payload that could be flight ready in 2020.
    
    The LUVMI sampling instrument will be tested in a highly representative environment including thermal, vacuum and regolith simulant and the integrated payload demonstrated in a representative environment.
    Abstract document

    IAC-17,A3,2B,10,x41392.brief.pdf

    Manuscript document

    IAC-17,A3,2B,10,x41392.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.