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  • Development of a Tool for Multi-Layer Insulation Manipulation and Handling

    Paper number

    IAC-16,E2,2,7,x35881

    Coauthor

    Mr. Martin Dullweber, University of Bremen, Germany

    Year

    2016

    Abstract
    Most active satellites run out of propellants before any defects that inhibit their functionality occur. Refueling those satellites with on-orbit servicing missions would allow for significant lifetime extensions. A NASA project report from 2010 estimates a number of about 140 satellites that will be put out of service by 2020 and would have profited from such an extension. Outlined here is the design and testing of a tool for the cutting and handling of multi-layer insulation used in the thermal design of satellites. This task is required to expose the fuel ports on traditional satellite designs, where on-orbit servicing was not intended, rendering it an important part of the refueling procedure. For this purpose, multiple concepts were developed and rated through a technical assessment as suggested by the Association of German Engineers (VDI) product development guidelines. The solution that was found to be the best fit to the requirements consists of a heating wire for thermal cutting and a holding utility based on gecko adhesion. The adhesive approach, while only holding on to the topmost layer of the thermal blanket, works due to a heat-sealing of the cutting edges, effectively fusing the layers of the cut-out into one piece. This tool has been manufactured as a prototype to perform multiple tests in which the functional reliability has been validated. Finally, a demonstration using a satellite replication and a robotic manipulator has been performed. Due to the very good cut quality, relatively easy implementation, great flexibility and a reliable connection between the holding utility and the created cut-out, the tool has to be considered as a viable option to perform (on-orbit) manipulations on a satellites thermal blanket.
    Abstract document

    IAC-16,E2,2,7,x35881.brief.pdf

    Manuscript document

    IAC-16,E2,2,7,x35881.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.