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  • eleonora, a 3U cubesat for the canadian satellite design challenge

    Paper number

    IAC-15,E1,3,8,x30090

    Author

    Ms. Constance Fodé, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mr. Jacopo Panerati, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mr. Alexandre Guay, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mrs. Prescilia Desroches, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mr. Marcello Valdatta, University of Bologna, Italy

    Coauthor

    Mr. Mark Smyth, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mr. Mathieu Lalonde, Ecole Polytechnique de Montreal, Canada

    Coauthor

    Mr. Niccolò Bellini, N.P.C. New Production Concept, Italy

    Coauthor

    Mr. Davide Rastelli, N.P.C. New Production Concept, Italy

    Coauthor

    Mr. Stefano Naldi, N.P.C. New Production Concept, Italy

    Coauthor

    Prof. Giovanni Beltrame, Ecole Polytechnique de Montreal, Canada

    Year

    2015

    Abstract
    In the paper we present the Eleonora mission. 
    Eleonora is a 3U cubesat designed by PolyOrbite, a joint team from Polytechnique Montreal (Quebec, Canada) and the University of Bologna (Italy) to compete in the 2012-2014 iteration of the educational programme known as the Canadian Satellite Design Challenge (CSDC).
    The satellite was designed to carry two payloads: a camera and a deorbiting system based on an aerodynamic drag sail. 
    The main mission of Eleonora is to use its camera to take photos of the Canadian Arctic for the Geocryolab (Laboratory of Geotechnics and Geomorphology of Cold Regions) of the University of Montreal. 
    The secondary mission of Eleonora is to perform a deorbiting manoeuvre using its deployable drag sail.
    In the context of the CSDC, an inter-university competition, the Eleonora mission was developed over a 20 months timeline.
    The two teams worked in their respective country but had regular meetings, via teleconference or in person, to review the project. 
    During this period, the two teams first ideated the mission, then designed, produced, integrated, and tested the 3U cubesat.
    The CSDC required Eleonora to undergo an informal preliminary design review, a critical design review, and a vibration test of the final design.
    At the end of the 2012-2014 CSDC, Eleonora obtained the third overall place among teams coming from ten of the major Canadian universities.
    A considerable success for the young student society PolyOrbite, created at Polytechnique Montreal in 2012 with the specific goal to recruit students who were passionate about space and willing to embark in the CSDC experience.
    The paper describes the entire experience of creating a cubesat mission with a team of graduate and undergraduate students coming from different countries: from the design of the satellite, to the results of the environmental tests performed at the David Florida Laboratory of the Canadian Space Agency, passing through the organizational issues and the lessons learned, with a view to the future of the programme.
    Abstract document

    IAC-15,E1,3,8,x30090.brief.pdf

    Manuscript document

    IAC-15,E1,3,8,x30090.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.