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  • Cost estimation of active debris removal

    Paper number

    IAC-12,A6,5,3,x14701

    Author

    Dr. Carsten Wiedemann, Technical University of Braunschweig, Germany

    Coauthor

    Mr. Sven Kevin Flegel, Technische Universität Braunschweig, Germany

    Coauthor

    Mr. Marek Moeckel, Technische Universität Braunschweig, Germany

    Coauthor

    Mr. Johannes Gelhaus, Technische Universität Braunschweig, Germany

    Coauthor

    Mr. Vitali Braun, Technische Universität Braunschweig, Germany

    Coauthor

    Mr. Christopher Kebschull, Technische Universität Braunschweig, Germany

    Coauthor

    Mr. Joerg Kreisel, JOERG KREISEL International Consultant (JKIC), Germany

    Coauthor

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

    Coauthor

    Prof. Peter Voersmann, Technische Universität Braunschweig, Germany

    Year

    2012

    Abstract
    The number of debris objects on some low Earth orbit (LEO) regions is high. There is a certain possibility that objects may collide with each other. Huge spent satellites or upper stages can be destroyed so that new debris is created. The new debris may in turn trigger further catastrophic collisions. Simulations show that an instability may exist in the LEO population. Consequently catastrophic collisions may become the driving mechanism for the increase in the number of debris in the future. In addition to the introduction of mitigation measures, active removal of already existing objects may be necessary. Target objects could be selected that pose a high risk. These are long-lived objects in LEO, usually near 800 km altitude, which have a large cross-sectional area and a high mass. For the mission, a removal satellite would be required. The satellite has to perform a rendezvous maneuver, a docking with the target object, and a direct de-orbiting of the target. Cost drivers are derived from the mission requirements for an active removal. The costs for development and production of the satellites hardware as well as for operations are estimated. A long-term simulation of the space debris environment is carried out. The results with or without active removal are examined. The costs of both scenarios are compared.
    Abstract document

    IAC-12,A6,5,3,x14701.brief.pdf

    Manuscript document

    IAC-12,A6,5,3,x14701.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.