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  • The International Berthing Docking Mechanism (IBDM): demonstrating full compliance to the International Docking System Standard (IDSS)

    Paper number

    IAC-15,B3,7,7,x30720

    Author

    Mr. Helder Dittmer, QinetiQ Space nv, Belgium

    Coauthor

    Mr. Oscar Gracia, European Space Agency (ESA), The Netherlands

    Coauthor

    Mr. Marco Caporicci, European Space Agency (ESA), The Netherlands

    Coauthor

    Mr. Bart Paijmans, QinetiQ Space nv, Belgium

    Coauthor

    Mr. David Meuws, QinetiQ Space nv, Belgium

    Year

    2015

    Abstract
    The International Docking System Standard (IDSS) is the result of a collaboration by the International Space Station (ISS) membership to establish a recommended standard docking interface to enable joint collaborative endeavors utilizing different spacecraft and on-orbit crew rescue operations. The purpose of the IDSS is to provide basic common design parameters to allow developers to independently design compatible docking systems. The IDSS defines the meshing geometry, the contact and in-orbit loads and the range of masses and Initial Contact Conditions of the mating spacecraft that a docking system, implementing the standard, shall comply to. 
    
    QinetiQ Space, under ESA contract, is currently building the International Berthing Docking Mechanism (IBDM), an androgynous low impact docking mechanism which features an actively controlled soft-capture system that is capable of docking and berthing large and small spacecraft, and is compatible with the IDSS definition. At the same time, NASA is also conducting the design and manufacturing of their NDS (NASA Docking System) compatible with the IDSS definition.  NASA is also outfitting the ISS with 2 International Docking Adapters (IDAs) to provide IDSS compatible docking ports for future commercial crew and other visiting spacecraft. 
    
    The paper describes the demonstration through simulation and testing of the compatibility of the IBDM with the meshing geometry, the structural contact loads and the broad range of masses and ICCs of the mating spacecraft defined by the IDSS. The presented testing is an important step in the preparation for operational use of the IBDM on one of the new generation vehicles servicing the ISS.
    Abstract document

    IAC-15,B3,7,7,x30720.brief.pdf

    Manuscript document

    IAC-15,B3,7,7,x30720.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.