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    No. 145 - Superior solar conjunction

    29 Oct 2010 12:00

    Report for the period 25 September to 22 October 2010

    This report covers 28 days of Rosetta mission operations. During the reporting period, the spacecraft has been going through a superior solar conjunction, which will end on 31 October. During this phase, the spacecraft was configured in active cruise mode, but with very limited ground station communications due to the effects of the Sun on the RF signal transmission. The NASA Deep Space Network (DSN) provided additional support to the radio science investigations during this phase.

    During the reporting period, mission operations were conducted using the ESA New Norcia (NNO) ground station and the DSS-15 (Goldstone, 34 metres), DSS-54 (Madrid, 34 metres), DSS-63 (Madrid, 70 metres) and DSS-65 (Madrid, 34 metres) NASA Deep Space Network (DSN) antennas.

    Main activities during reporting period

    DoY Date Pass Activity
    270 27-Sep-2010 NNO 2407 Monitor
    273 30-Sep-2010 NNO 2410 Monitor
    275 2-Oct-2010 DSS-54 2412 Monitor
    276 3-Oct-2010 DSS-54 2413 Monitor
    277 4-Oct-2010 DSS-65 2414
    NNO 2414
    Monitor
    278 5-Oct-2010 DSS-15 2415 Monitor
    279 6-Oct-2010 DSS-65 2416 Monitor
    280 7-Oct-2010 DSS-54 2417
    NNO 2417
    Monitor
    281 8-Oct-2010 DSS-65 2418 Monitor
    282 9-Oct-2010 DSS-65 2419 Monitor
    283 10-Oct-2010 DSS-63 2420 Monitor
    284 11-Oct-2010 DSS-63 2421
    NNO 2421
    Monitor
    285 12-Oct-2010 DSS-63 2422 Monitor
    287 14-Oct-2010 DSS-63 2424
    NNO 2424
    Monitor
    288 15-Oct-2010 DSS-63 2425 Monitor
    289 16-Oct-2010 DSS-63 2426 Monitor
    290 17-Oct-2010 DSS-63 2427 Monitor
    291 18-Oct-2010 DSS-63 2428
    NNO 2428
    Monitor
    292 19-Oct-2010 DSS-63 2429 Monitor
    294 21-Oct-2010 NNO 2431 Monitor
    295 22-Oct-2010 DSS-63 2432 Monitor

    DoY = Day of year

    At the end of the reporting period on 22 October, Rosetta was 657 million km from Earth (4.39 AU); the one-way signal travel time was 36 min 32 sec (2192 sec). The spacecraft’s distance from the Sun was 509 million km (3.4 AU).

    Spacecraft

    Attitude and orbit control system
    The spacecraft has been using three reaction wheels for attitude control since 15 July, when reaction wheel B was switched off to conserve power; nominally, it will not be restarted until after the end of deep-space hibernation. Since 27 August, reaction wheel C has been exhibiting very noisy friction torque; its behaviour appears to be degrading and is being carefully monitored.

    Payload Status
    ALICE The instrument is currently OFF
    CONSERT The instrument is currently OFF
    COSIMA The instrument is currently OFF
    GIADA The instrument is currently OFF
    MIDAS The instrument is currently OFF
    MIRO The instrument is currently OFF
    OSIRIS The instrument is currently OFF
    ROSINA The instrument is currently OFF
    RPC The instrument is currently OFF
    RSI The USO is ON/muted since 3 February 2010 (DoY 032/2010). Experiment activities are being supported by means of dedicated ground station measurements.
    VIRTIS The instrument is currently OFF
    Lander (Philae) The instrument is currently OFF
    SREM The instrument is ON with standard settings since 3 February 2010 (DoY 032/2010).

    Future milestones

    The angular separation between the spacecraft and the Sun is now slowly increasing, reducing the negative effect on RF communications. The dumping of mass memory will be resumed at the beginning of the next reporting period and the conjunction phase will formally end on 31 October.

    After this phase, spacecraft activities will focus on the last payload checkout and the preparation of the instruments for the hibernation phase. These activities will be conducted between mid-November and mid-December.

    The first rendezvous manoeuvre is planned for the second half of January 2011, with the first burn leg on 17 January. Due to its magnitude, this manoeuvre has been split into five nominal burns plus an optional extra one in the event that a final correction is needed.

    ---
    Legal disclaimer
    This report is based on the ESOC mission operations report, WOR #145.  Please see the copyright section of the legal disclaimer (linked from the home page http://sci.esa.int) for terms of use.


    Last Update: 05 Mar 2012

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