A communication link for the transfer of data between the crew cabin and payload bay of the Shuttle is proposed. The configuration of the system, which is to transmit data optically through the Shuttle cabin window, is described. The effects of temperature cycling and cosmic radiation on optical fibers, the cable, connectors, and lenses, and of vibrations during a mission on the alignment of collimating lenses at the window are investigated. Consideration is given to determining the optimum design for the optical fiber and the optimum system operation wavelength for transmission through the aft Orbiter window and the payload environment.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An optical communication link on the Shuttle


    Beteiligte:
    Grady, Jane L. (Autor:in)

    Erscheinungsdatum :

    01.01.1986


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    An optical communication link on the Shuttle

    Grady, J.L. | Tema Archiv | 1986


    10 GBPS Shuttle-to-Ground Adjunct Communication Link Capability Experiment

    Ceniceros, J. M. / Sandusky, J. V. / Hemmati, H. et al. | British Library Conference Proceedings | 1999


    10 Gbps Shuttle-to-Ground Adjunct Communication Link Capability Experiment

    Hemmati, H. / Sandusky, J. / Ceniceros, J. | NTRS | 1999


    FIRST SHUTTLE-MIR LINK-UP

    Kidger, Neville | Online Contents | 1995


    Articles - High Rate Shuttle Data Link

    Engelberg | Online Contents | 2000