A series of seven gravity-gradient dynamics experiments is proposed utilizing the Radio Astronomy Explorer (RAE-B) spacecraft in lunar orbit. It is believed that none of the experiments will impair the spacecraft structure or adversely affect the continuation of the scientific mission of the satellite. The first experiment is designed to investigate the spacecraft dynamical behavior in the absence of libration damper action and inertia. It requires stable gravity-gradient capture of the spacecraft in lunar orbit with small amplitude attitude librations as a prerequisite. Four subsequent experiments involve partial retraction, ultimately followed by full redeployment, of one or two of the 230-meter booms forming the lunar-directed Vee-antenna. These boom length change operations will induce moderate amplitude angular librations of the spacecraft.


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    Title :

    Proposed gravity-gradient dynamics experiments in lunar orbit using the RAE-B spacecraft


    Contributors:

    Publication date :

    1973-05-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English


    Keywords :






    Orbit Control for a Spacecraft via the Gravity Gradient Force

    Watanabe, Y. / Nakamura, Y. / International Astronomical Federation | British Library Conference Proceedings | 1998