The authors present an Orbital Maneuvering Vehicle space station communications systems design approach which is intended to satisfy the stringent link requirements. The operational scenario, system configuration, signal design, antenna system management, and link performance analysis are discussed in detail. It is shown that the return link can transmit up to 21.6 Mb/s and maintain at least a 3 dB link margin through proper power and antenna management control at a maximum distance of 37 km. It is suggested that the proposed system, which is compatible with the space station multiple-access system, can become a model for other space station interoperating elements or users to save the development cost and reduce the technical and schedule risks.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Orbital Maneuvering Vehicle space station communications system design


    Weitere Titelangaben:

    Entwicklung eines Kommunikationssystems fuer Weltraumstationen mit orbital manoevrierten Fahrzeugen


    Beteiligte:
    Tu, K. (Autor:in) / Loh, Y.C. (Autor:in) / Kuo, Y.S. (Autor:in) / Arndt, D. (Autor:in) / Novosad, S.W. (Autor:in)


    Erscheinungsdatum :

    1988


    Format / Umfang :

    5 Seiten, 6 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Orbital Maneuvering Vehicle space station communications design

    Arndt, D. / Novosad, S. W. / Tu, K. et al. | NTRS | 1988




    Orbital Maneuvering system design evolution

    Gibson, C. / Humphries, C. | NTRS | 1985


    Orbital maneuvering vehicle attitude control system

    PARRY, PAUL / GOLUB, ALEX / SOUTHWOOD, DANA | AIAA | 1989