The heart of the spacecraft downlink is the flight data subsystem (FDS). The FDS combines the functions of science and engineering measurement control. The FDS can generate six principal telemetry formats, each of which may be transmitted directly to earth. Spacecraft engineering subsystems are considered, giving attention to the power subsystem, the attitude control subsystem, the propulsion subsystem, devices for temperature control, and the tracking subsystem. The mission operations system is also discussed together with the flight plan.


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    Titel :

    The 1973 Mariner mission to Venus and Mercury. II


    Beteiligte:
    Hooke, A. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Mariner Venus/Mercury 1973 preliminary mission design

    Beerer, J. G. / Bourke, R. D. | NTRS | 1970



    Mariner Venus Mercury, 1973

    Wilson, J. H. | NTRS | 1973


    Mariner mission to Venus and Mercury in 1973

    Beerer, J. G. / Bourke, R. D. | NTRS | 1971


    Mariner Venus/ Mercury 1973 Study

    C. W. Cole / P. K. Eckmann | NTIS | 1969