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  • Technological Challenges For Manufacturing LARES Satellite

    Paper number

    IAC-09.C2.I.5

    Author

    Prof. Antonio Paolozzi, University of Rome "La Sapienza", Italy

    Coauthor

    Prof. Ignazio Ciufolini, Università del Salento, Italy

    Coauthor

    Mr. Francesco Passeggio, OMPM srl, Italy

    Coauthor

    Mr. Laura Caputo, OMPM srl, Italy

    Year

    2009

    Abstract
    Due to the peculiar alloy used for LARES satellite some concerns arise about the machinability of the material. Although several producers can provide several types of tungsten alloy, and there is a market that uses bulk tungsten material, to our knowledge this material, very seldom used in space, was never machined with tight manufacturing tolerances and severe surface finish. Consequently several tests for machinability and polishing have been performed. Particular care has been adopted for manufacturing spherical cavities that are used to interface the separation system. Also the screws and the retainer ring for the cube corner reflector mounting system are difficult items to be manufactured in tungsten alloy, being the screw shaft and the ring thickness very small. Special tool for grabbing and moving the semifinished sphere on the tooling machines will be designed. The industrial production process including programming, manufacturing and testing will be described. Some  breadboards have been manufactured to address possible manufacturing problems.
    Abstract document

    IAC-09.C2.I.5.pdf

    Manuscript document

    IAC-09.C2.I.5.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.