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  • MASCOT, the small mobile asteroid landing package on its piggyback journey to 1999 JU3: pre-launch and post-launch activities

    Paper number

    IAC-15,A3,4,6,x30774

    Author

    Mr. Christian Ziach, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Dr. Volodymyr Baturkin, DLR (German Aerospace Center), Germany

    Coauthor

    Dr. Tra-Mi Ho, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Mr. Christian Grimm, Germany

    Coauthor

    Mr. Jan Thimo Grundmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Mrs. Caroline Lange, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Ms. Nawarat Termtanasombat, Luleå Technical University, Germany

    Coauthor

    Ms. Wejmo Elisabet, DLR, German Aerospace Center, Germany

    Coauthor

    Mr. Ross Findlay, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Dr. Josef Reill, Deutsches Zentrum fuer Luft- und Raumfahrt (DLR), Germany

    Coauthor

    Mr. Michael Lange, DLR (German Aerospace Center), Germany

    Coauthor

    Mr. Olaf Mierheim, DLR (German Aerospace Center), Germany

    Coauthor

    Dr. Jens Biele, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Mr. Christian Krause, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Dr. Stephan Ulamec, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Ms. Belinda Borgs, Deutsches Zentrum fuer Luft- und Raumfahrt (DLR), Germany

    Coauthor

    Dr. Matthias Grott, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Prof. Ralf Jaumann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Coauthor

    Mrs. Muriel Deleuze, Centre National d'Etudes Spatiales (CNES), France

    Coauthor

    Prof. Jean-Pierre Bibring, IAS, France

    Coauthor

    Dr. Hans-Ulrich Auster, Technische Universität Braunschweig, Germany

    Year

    2015

    Abstract
    Since December 2014 the Japanese spacecraft Hayabusa-II is on its journey to asteroid 1999 JU3. Like its famous predecessor it is foreseen to study and return samples from its target body. This time, the mother spacecraft has several small passengers. One of them is a compact landing package called MASCOT (Mobile Asteroid surface SCOuT), which has been developed by the German Aerospace Centre (DLR) and the Centre National d'Etudes Spatiales (CNES). Once having been released from its mother-spacecraft's cradle, MASCOT will descend to the asteroid and after a few bounces will come to rest at a certain location on the surface. Sitting on the surface, it will perform its scientific investigations of the asteroids surface structure, mineralogical and physical properties, thermal behaviour and magnetic effects by using its suite of four scientific instruments: a spectrometer (MicrOmega, IAS Paris), a camera (CAM, DLR Berlin), a radiometer (MARA, DLR Berlin) and a magnetometer (MAG, TU Braunschweig). These payload operations are made possible, amongst others, by a clever thermal subsystem design specifically devised to cope with the contrasting requirements of cold cruise and hot on-surface operations and a primary battery optimizing mass versus energy output. A mobility mechanism realizes locomotion on the surface 
    supported by an according attitude and motion sensing system and an intelligent autonomy manager, which is implemented in the onboard Software, can operate MASCOT when ground intervention is not available.
    
    In a nutshell, with its many challenging technical hurdles that have been solved, the MASCOT lander can serve as a benchmark for extremely lightweight (~10kg), highly integrated mobile small body landing systems with onboard autonomy and high science output.
    
    This paper will summarize the mission and system development. We will provide an overview over the final capabilities of the system as well as discuss the latest challenging pre-launch activities and tests. Further a summary and an outlook regarding the already performed as well as upcoming post-launch activities will follow. Lessons have been learned and will be told to be ready for future upcoming missions in the frame of small body exploration.
    Abstract document

    IAC-15,A3,4,6,x30774.brief.pdf

    Manuscript document

    IAC-15,A3,4,6,x30774.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.