metop data sheet

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  • 7/29/2019 Metop Data Sheet

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    MetOp A, B, & C are te rst European polar orbiting satellites dedicated to operational meteorology.

    Designed and developed by Astrium for the European Space Agency (ESA) and the European

    Organisation for te Exploitation of Meteorological Satellites (EUMETSAT), tese satellites provide

    meteorological data for te morning service, to complement te data collected by te US National

    Oceanic and Atmosperic Administration (NOAA) satellites, wic cover te afternoon orbit. From

    their polar orbit, at a much lower altitude than the other European geostationary meteorological

    satellites, te MetOp satellites are ideally located to gater ig resolution Eart Observation information,

    as well as accurate atmosperic data.

    Te MetOp A satel lite was launced in October 2006, and declared operational on 15th May 2007.

    Launc of MetOp B will take place in 2012 and MetOp C in 2017, at ve year intervals, so as to ensurete continuity of operational service over a period of about 15 years.

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    For more information please contact:

    Jean-Paul Gardelle

    MetOp Project Manager

    Eart Observation, Navigation & Science Division

    Astrium sAtellites

    Toulouse

    France

    PhONE: +33 (0) 5 62 19 69 93

    EMAIL: [email protected]

    www.astrium.eads.net

    Customer European Space Agency and EUMETSAT

    Mission Meteorological

    Spacecraft Characteristics

    Dimensions 6.6 x 6.3 x 5.0 metres (deployed conguration witout solar array)

    Launch Mass 4100 kg (at launc)

    Power 3800W (End of Life)

    Design Lifetime 5 years

    Orbit Near-polar sun-syncronous, Mean altitude 830km

    Local solar time 09.30, descending node, 29-day repeat cycle

    Payload Characteristics

    Number of Instruments 12

    Instrument Mass 900 kg

    Instrument Power 950 W

    Instrument Data Rate 2600 Kbps

    Instruments

    Advanced Very hig Resolution Radiometer (AVhRR) Imaging Radiometer, 6 cannels (0.6-12m)

    hig-resolution Infrared Radiation Sounder (hIRS) Sounder, 19 infrared cannels (3.8-15) 1 visible cannel

    Advanced Microwave Sounding Units (AMSU-A1&A2) Microwave sounder, 15 cannels (23-90Gz)

    Microwave humidity Sounder (MhS) Microwave sounder, 5 cannels (89-183Gz)

    Advanced Data Collection System (A-DCS) UhF receiver and signal processor

    Infrared Atmosperic Sounding Interferometer (IASI) Infrared Micelson interferometer (3.6-15)

    Advanced Scatterometer (ASCAT) Pulsed radar in C-band

    Global Ozone Monitoring Experiment-2 (GOME) Nadir-viewing UV and visible spectrometer

    GNSS Receiver for Atmosperic Sounding (GRAS) Radio occultation receiver

    Searc and Rescue Monitor (S&R) VhF/UhF transponder and signal processor

    Space Environment Monitor (SEM) Multi-cannel carged particles spectrometer

    The Mission

    MetOp A, B & C will provide global coverage of te Eart wit detailed observations wic will be used for botmeteorology and climatology applications. Te MetOp mission includes several enancements over te existing

    NOAA meteorologica l polar satellites, suc as te introduction of advanced sounding and surface wind measurement

    capabilities, advanced global ozone monitoring, direct data broadcast services, and te capability to obtain full

    resolution data from te complete orbit. In addition, te coice of te orbit parameters as been optimised for

    te European weater prediction models.

    Eac satellite will carry a set of 12 complementary instruments. Tese comprise sounding (microwave and infra-

    red), imagery (ig resolution radiometer images), data collection from buoys and oter platforms, ozone monitoring,

    wind scatterometry (wind speed and direction over te ocean), space environment monitoring (carged particle

    uxes), as well as a umanitarian service (searc and rescue). Some of tese instruments are common to bot

    te MetOp and te US satellites; for example te Microwave humidity Sounder (MhS) a 5-cannel sel f-calibrating

    microwave scanning radiometer wic was developed by Astrium.

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