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  • A Logistic System based on Momentum Exchange Tethers for Earth-Moon cargo transportation

    Paper number

    IAC-06-D3.2.06

    Author

    Ms. Manuela Aguzzi, Politecnico di Milano, Italy

    Coauthor

    Prof. Matthew Cartmell, University of Glasgow, United Kingdom

    Coauthor

    Dr. Gianmarco Radice, University of Glasgow, United Kingdom

    Coauthor

    Dr. Massimiliano Vasile, University of Glasgow, United Kingdom

    Coauthor

    Mr. Marco Villanti, Italy

    Coauthor

    Dr. Maria Antonietta Perino, Thales Alenia Space, Italy

    Year

    2006

    Abstract
    The main function of logistic systems is to provide safe and reliable transportation of crew and cargo (propellant, supplies for crew, different kind of consumable…) to and from the Moon. Advanced logistic systems should also offer transportation of in-situ products (such as oxygen and propellant) from Moon to Earth.
    Moreover logistic systems should support the lunar-base needs during its entire life cycle, and allow its growth and expansion providing supply form Earth. This would require a permanent transportation system from the Earth to the Moon and back. Last study performed by NASA (the ESAS study) foresees that crew and cargo should be launched separately. Following this trail, a reliable and economic logistic system based on momentum-exchange tethers had been studied as a potential candidate for a continuous transportation system in view of a Moon settlement.
    This paper presents the results of a study performed under ESA-Alcatel-Alenia contract and developed by a multidisciplinary team of Aerospace Engineers, Mechanical Engineers and Industrial Designers.
    A general scenario is defined in which the Momentum Exchange Tethers (MET) can serve as the main transportation system.  A particular container (here called transportation egg) is proposed which interfaces with the MET and allows an efficient stowage of goods and facilities. An accurate study has been conducted for the accommodation of payload and instrumentations inside the egg. Also filling/emptying procedure and logistics to ease payload extraction on the lunar surface has been analyzed. Moreover the egg provides protection from external hazards and contamination, plus the required devices to land safely on the surface of the moon.   
    
    Abstract document

    IAC-06-D3.2.06.pdf

    Manuscript document

    IAC-06-D3.2.06.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.