Since 1975, MECANEX S.A. has been manufacturing components for solar array drives and mechanisms used in space applications. In 1991, work was started in an early phase C (Engineering Model) on a Coarse Pointing Mechanism Assembly (CPMA) for the Semiconductor-laser Inter-satellite Link EXperiment (SILEX). This paper deals with the history, the evolution, and the lessons learned from taking over a pre-design in 1991 to the delivery of last flight models (FM 5 & 6) in 1995.


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    Titel :

    Coarse pointing mechanism assembly for satellite interlink experiment


    Beteiligte:
    Maeusli, P. A. (Autor:in) / Ivorra, M. T. (Autor:in) / Gass, V. (Autor:in) / Berthoud, J. F. (Autor:in)


    Erscheinungsdatum :

    01.05.1996


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Coarse Pointing Mechanism Assembly for Satellite Interlink

    Maeusli, P.-A. / Ivorra, M.-T. / Gass, V. et al. | British Library Conference Proceedings | 1996



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    A Coarse Pointing Assembly for Optical Communication

    Szekely, G. / Blum, D. / Humphries, M. et al. | NTRS | 2010


    Contraves optical terminal-coarse pointing assembly (CPA)

    Mussett, D. J. / Humphries, M. E. / Henzelin, F. et al. | British Library Conference Proceedings | 2003