The launch of the WIND spacecraft will place the satellite into a sunside apogee double-lunar swing-by orbit for a period of one year, after which WIND may be transferred to a Sun-Earth L1 Halo orbit. Information is presented in tabular form on the following topics: Deep Space Network support; frequency assignments, telemetry, command, and ranging.


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    Title :

    International Solar Terrestrial Physics (ISTP) Wind Mission


    Contributors:
    R. Sanford (author) / K. O. Sizemore (author)

    Publication date :

    1991


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    International Solar Terrestrial Physics (ISTP) WIND Mission

    Sanford, R. / Sizemore, K. O. | NTRS | 1991




    International Solar Terrestrial Physics (ISTP) Program

    R. Sanford / D. Muhonen / K. O. Sizemore | NTIS | 1991


    International Solar Terrestrial Physics (ISTP) program

    Sanford, R. / Muhonen, D. / Sizemore, K. O. | NTRS | 1991