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  • MORE: an advanced tracking experiment for the exploration of Mercury with the mission BepiColombo.

    Paper number

    IAC-06-C1.6.04

    Author

    Prof. Luciano Iess, University of Rome "La Sapienza", Italy

    Coauthor

    Mr. Sami W. Asmar, Jet Propulsion Laboratory, United States

    Coauthor

    Prof. Paolo Tortora, University of Bologna, Italy

    Year

    2006

    Abstract

    Precise microwave tracking of interplanetary spacecraft has been a crucial tool in solar system exploration. Not only range and range rate measurements are the main observable quantities in spacecraft orbit determination and navigation, but they have been widely used to refine the dynamical model of the solar system and to probe planetary interiors. Thanks to the use of Ka-band and multifrequency radio links, a significant improvement in microwave tracking systems has been demonstrated by the radio science experiments of the Cassini mission to Saturn. The Cassini radio system has been used to carry out the most accurate test of General Relativity to date.

    Further developments in the radio instrumentation have been recently started for the MORE experiment, selected for the ESA mission to Mercury, BepiColombo. MORE addresses the mission’s scientific goals in geodesy, geophysics and fundamental physics. In addition, MORE will carry out a navigation experiment, aiming to a precise assessment of the orbit determination accuracies attainable with the use of the novel instrumentation.

    The key instrument is a Ka/Ka band digital transponder enabling a high phase coherence (to a level of 10 −15 over 1000 s integration time) between uplink and downlink carriers and supporting a wideband (20 MHz) ranging tone. The onboard instrumentation is complemented by a ground system based upon the simultaneous transmission and reception of multiple frequencies at X and Ka-band. The new wideband ranging system (WBRS) is designed for an end-to-end accuracy of 20 cm using integration times of a few seconds. Two-way range rate measurements are expected to be accurate to 3 micron/s, thanks to nearly complete cancellation or calibration of the propagation noise from interplanetary plasma and troposphere. We review the experimental configuration of the experiment and outline its scientific goals and expected results.

    Abstract document

    IAC-06-C1.6.04.pdf

    Manuscript document

    IAC-06-C1.6.04.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.