Artemis

From: Bruno Tilgner (Bruno_Tilgner@compuserve.com)
Date: Thu Jul 19 2001 - 13:28:06 PDT

  • Next message: Paul Gabriel: "obs 20jul 01201.16"

    The following ESA press release may be of interest to SEESAT.
    
    
    Press Release N°43-2001 - ESA starts recovery of Artemis
    
    Paris, 19 July 2001
    Press Release
    N°43-2001
    
    ESA starts recovery of Artemis 
    
    ESA's Artemis telecommunications satellite is fully under the control of
    the Altel (Alenia Spazio-Telespazio) operations team and system engineers
    in Fucino, Italy, supported by a team of ESA specialists, after a
    successful first orbit-raising manoeuvre last night.
    
    The satellite was launched by an Ariane 5 on Thursday 12 July from Kourou
    but was left in a degraded orbit due to a malfunction in the launcher's
    upper stage. Artemis was injected into an orbit with a perigee of 590 km,
    an apogee 17 487 km and inclination of 2.94°, compared to expected values
    of 858 perigee, 35 853 apogee, and 2° inclination. Since injection into
    orbit the spacecraft's behaviour has been nominal. The solar arrays were
    partially deployed, according to plan, some two hours after launch and
    started delivering the power required for operation. Several calibrations
    and simulated apogee firings have been performed in the last few days to
    prepare for the orbit manoeuvres described below.
    
    The recovery strategy adopted aims to bring the satellite to the nominal
    geostationary position and to maintain chemical propellant and xenon (the
    gas used for the electrical ion-propulsion system) to maximise the
    lifetime of the spacecraft, originally planned to last 10 years.
    
    The combined ESA/Alenia Spazio-Telespazio team has jointly selected a
    four-step strategy for bringing Artemis from the current non-nominal orbit
    to the geostationary orbit, as follows:
    
    Step 1: The apogee boost motor (using chemical propulsion) is operated
    during several perigee passes (at the shortest distance from Earth) to
    increase the apogee (the maximum distance from Earth) to about 31 000 km.
    The perigee will not be raised by very much. Ground stations at Fucino
    (Italy), Malindi (Kenya), Perth (Australia), Goldstone (USA) and Kourou
    (French Guiana) will monitor the satellite.
    
    Step 2: The elliptical orbit is then  circularised by a number of apogee
    and perigee manoeuvres  resulting in a quasi-circular parking orbit with
    the satellite at 31 000 km above the Earth and an orbit duration of about
    18 hours. On completion of this step, the solar arrays will be fully
    deployed, as will the antenna reflectors. The satellite will then be in
    nominal mode, while not yet in geostationary orbit.
    
    Step 3: With the satellite in the parking orbit, nominal spacecraft
    commissioning (activation and checking that all satellite elements are
    operating correctly) will be carried out, as far as is possible, in this
    sub-geostationary orbit.
    
    Step 4:	The satellite will then  be "spiralled" from the parking orbit to
    the nominal geostationary orbit using the satellite's electrical
    ion-propulsion system.
    
    The first apogee boost motor burn at perigee was successfully accomplished
    yesterday evening (18  July) between 17:19 and 17:39 CEST. Ground
    controllers reported that all went well and that the satellite has now
    been raised to an apogee altitude of 19 164 km  (the perigee moving to 609
    km, with no change in the inclination of 2.9°).
    
    The end of step 2, i.e. arrival at the parking orbit, is planned for the
    next few days. Step 3 will last about 2 months, during which the
    commissioning tests will be performed and preparations will be made for
    raising the orbit. Step 4 is expected to start at end of September and
    will last  several months.
    
    This recovery scenario is the one which offers the best chances of
    bringing the satellite from the degraded injection orbit to the nominal
    geostationary position and saving enough chemical fuel and xenon to
    support some years of nominal operation. The amount of fuel and the
    resulting remaining lifetime can be predicted only after completion of
    step 2, albeit with some uncertainty.
    
    The recovery activities involve a number of unusual operations which could
    not be planned for in advance. A particular case in point is the use of
    the electrical ion-propulsion system, for which a new mode of operation
    has to be defined.
    
    The next progress report will be published on completion of step 2.
    
    For further information:
    ESA Media Relations Office
    Franco Bonacina
    Tel: +33.(0)1.5369. 7713
    Fax: +33.(0)1.5369.7690
    
    See also http://www.esa.int
    
    Note to broadcasters:
    A Video News Release for TV Broadcasters will be available on Friday 20
    July from 04:30-04:45 GMT on Eutelsat W1. For more information on the TV
    transmission consult http://www.television.esa.int or contact Medialink:
    +44.207.554.2704
    
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